Monday September 15th Morning Sessions

From 0700                                                                                                REGISTRATION

 0900 - 0930                                                                                           OPENING SESSION

 0930 - 1030                             ICAS DANIEL & FLORENCE GUGGENHEIM MEMORIAL LECTURE (INVITED) - Chairman: F. Abbink, ICAS President, The Netherlands

Prof. E. H. Dowell, Duke Univ., USA: REDUCED ORDER MODELS IN UNSTEADY AERODYNAMIC MODELS, AEROELASTICITY AND MOLECULAR DYNAMICS
(
ICAS 2008-0.1)

 

1030 - 1100                                                                                                        BREAK

1100 - 1130

 

1130 - 1200

1200 - 1230

 

 

 

 

 

 

 

 

 

 

 

 

 

ICAS 2008-1.1 MDO and its application: Chairs: M. Spiek, DLR, DE; J. Nixon, Georgia Tech., US

ICAS 2008-1.1.1

MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL DEVELOPMENT USING GENETIC ALGORITHM

C.-G. Pak, W. Li

NASA, USA

ICAS 2008-1.1.2

UNCERTAINTIES AT THE CONCEPTUAL STAGE: MULTILEVEL MULTIDISCIPLINARY DESIGN AND OPTIMIZATION APPROACH

M. Ravachol, Y. Deremeaux, Q. V. Dinh, et al

Dassault-Aviation, France

ICAS 2008-1.1.3

MULTI-DISCIPLINARY DESIGN EXPLORATION FOR WINGLET

K. Takenaka, K. Hatanaka, K. Nakahashi*

Mitsubishi Aircraft Corporation, Japan; *Tohoku Univ.,

ICAS 2008-2.1 Turbulent and Separated Flow: Chairs: R. Cosner, The Boeing Company, US

ICAS 2008-2.1.1

A HYBRID, DYNAMIC LARGE EDDY SIMULATION METHOD

C. Winkler, M. Mani, A. Dorgan

The Boeing Company, USA

ICAS 2008-2.1.2

HIGH-ORDER LARGE EDDY SIMULATION AROUND 2-D AEROFOIL WITH HIGH-LIFT DEVICE

T. Sumi, T. Kurotaki, J. Hiyama

JAXA, Japan

ICAS 2008-2.1.3

A STUDY OF SHEAR LAYER SUB-STRUCTURES IN LEADING EDGE VORTICES USING LASER DOPPLER VELOCIMETRY

J. D. Butler

Clarkson Univ., USA

ICAS 2008-3.1 Special Aerodynamic Problems: Chairs: B. Barzegar, Airbus, UK

ICAS 2008-3.1.1

ESTIMATION OF SUPERSONIC STAGE SEPARATION AERODYNAMICS OF WINGED-BODY LAUNCH VEHICLES USING RESPONSE SURFACE METHODS

G. Erickson, R. Deloach

NASA, USA

ICAS 2008-3.1.2

PROPELLER SLIPSTREAM INVESTIGATION USING THE FOKKER F27 WIND TUNNEL MODEL WITH FLAPS DEFLECTED

M. J. T. Schroijen, L. L. M. Veldhuis, R. Slingerland

TU Delft, Netherlands

ICAS 2008-3.1.3

THE APPLICATION OF SEMI-EMPIRICAL STORE RELEASE SIMULATION FOR THE OPTIMIZATION OF GRID SURVEY WIND TUNNEL TESTING

M. van der Steen, D. M. Orchard, F. C. Tang

National Research Council, Canada

ICAS 2008-4.1 Rocket Propulsion: Chairs: Y. Ibrahim, NRC, CA

ICAS 2008-4.1.1

PERFORMANCE ANALYSIS OF A 3D SCRAMJET INTAKE

B. U. Reinartz

RWTW Aachen Univ., Germany

ICAS 2008-4.1.2

PULSATING COMBUSTION OF AN ORGANIC GEL-FUEL DROPLET AND ITS INFLUENCE ON THE THERMAL FIELD OF A SPRAY DIFFUSION FLAME

A. Kunin, J. B. Greenberg, B. Natan

Technion, Israel

ICAS 2008-4.1.3

TURBULENCE MODELING S AND APPLICATIONS TO AEROSPIKE PLUG NOZZLE

M. Pires

Instituto Militar de Engenharia, Brazil

ICAS 2008-5.1 Flight Modelling I: Chairs: K. Rein-Weston, The Boeing Company, US

ICAS 2008-5.1.1 INVITED

A RAPID SCENARIO GENERATION TOOL FOR REPEATABLE SIMULATED TRAFFIC CONFLICTS IN FLIGHT SIMULATION

J. Gauci, D. Zammit-Mangion

Cranfield Univ., UK

ICAS 2008-5.1.2

CESSNA CITATION CJ1 FLIGHT TEST DATA GATHERING AND LEVEL-C SIMULATOR MODEL DEVELOPMENT

K. Hui, L. Auriti, J. Ricciardi

NRC, Canada

ICAS 2008-5.1.3

MODELING OF THE VISUAL APPROACH TO LANDING USING NEURAL NETWORKS AND FUZZY SUPERVISORY CONTROL

J. O. Entzinger

Univ. of Tokyo, Japan

ICAS 2008-6.1 Subsystems & Equipments Reliability: Chairs: A. Sinha, RMIT, AU

ICAS 2008-6.1.1

RELIABILITY STUDY OF POWER MODULE BY STOCHASTIC UNCERTAINTY METHOD FOR AN AERONAUTICAL APPLICATION

A. Micol, T. Lhommeau*, R. Meuret**, et al

ENIT-LGP, France; *PEARL, Alstom Transport Tarbes, France; **Hispano-Suiza, France

ICAS 2008-6.1.2

HEALTH MONITORING FOR COMMERCIAL AIRCRAFT SYSTEMS

K. W. Przytula, D. Allen, J. Vian*, et al

HRL Labs., LLC, USA; *The Boeing Company, USA

ICAS 2008-6.1.3

HIGH EFFICIENCY, HIGH RELIABILITY 2 KW INVERTER FOR AERONAUTICAL APPLICATION

S. Vieillard, R. Meuret

Hispano-Suiza, France

ICAS 2008-7.1 Composite Structures: Chairs: A. Blom, FOI, SE

ICAS 2008-7.1.1

PROBABILISTIC MODELING OF STRUCTURAL / AEROELASTIC LIFE CYCLE FOR RELIABILITY  EVALUATION OF DAMAGE TOLERANT COMPOSITE STRUCTURES

A. V. Styuart, K. Y. Lin, E. Livne

Univ. of Washington, USA

ICAS 2008-7.1.2

RESEARCH ON FAILURE CRITERION FOR COMPOSITE MATERIALS IN OPTIMIZATION

W. Cheng, D. Cui*

BUAA, China; *AVIC II, China

ICAS 2008-7.1.3

A MULTI-SCALE “MORPHOLOGICAL APPROACH” FOR MODELING THE NON LINEAR BEHAVIOR OF PROPELLANT-LIKE MATERIALS

C. Nadot-Martin, S. Dartois, A. Dragon, et al

ENSMA, France

ICAS 2008-8.1 UAS Integration into Airspace: Chairs: T. Ginn, NASA, US; S. Baillie, NRC, CA

ICAS 2008-8.1.1

REAL TIME SIMULATION OF INTEGRATION OF UAV'S INTO AIRSPACE

D -R. Schmitt, S. Kaltenhäuser, B. Keck

DLR, Germany

ICAS 2008-8.1.2

NATIONAL TECHNOLOGY PROJECT 'OUTCAST' ON UAV SENSE AND AVOID

M. Selier, M. Stuip, R. P. M. Verhoeven

NLR, Netherlands

ICAS 2008-8.1.3 (AIAA 2008-8967)

LARGE UAS OPERATIONS IN THE NAS - THE NASA 2007 WESTERN STATES FIRE MISSIONS

G. P. Buoni, K. M. Howell

NASA, USA

ICAS 2008-9.1 Aircraft Onboard Security: Chairs: A. Franzoni, Superjet International, IT

ICAS 2008-9.1.1

SECURITY ARCHITECTURE AND FORMAL ANALYSIS OF AN AIRPLANE SOFTWARE DISTRIBUTION SYSTEM

D. von Oheimb, M. Maidl, R. Robinson*

Siemens AG, Germany; *Boeing Phantom Works, USA

ICAS 2008-9.1.2

THREAT ASSESSMENT AND RESPONSE MANAGEMENT SYSTEM TARMS: AN ON-BOARD AIRCRAFT SECURITY SYSTEM

A. J. J. Lemmers

NLR, Netherlands

ICAS 2008-9.1.3

SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES

K. Sampigethaya, R. Poovendran*, M. Li**, et al

Univ. of Washington & Boeing Phantom Works, USA; *Univ. of Washington, USA; **Boeing Phantom Works, USA

ICAS 2008-10.1 Lighter-Than-Air Aircraft: Chairs: M. Conners,  Booz-Allen-Hamilton, US

ICAS 2008-10.1.1 (AIAA 2008-8850)

AIRSHIP TRANSPORT OPERATIONAL MANAGEMENT IN NORTHERN LATITUDES

R. Hochstetler, A. Sarma, N. Ahmad

SAIC, USA

ICAS 2008-10.1.2 (AIAA 2008-8851)

LOW COST TRANS-RIVER AERIAL-FERRY USING A NOVEL LTA SYSTEM

S. Banerjee, A. A. Raina, R. S. Pant

IIT, India

ICAS 2008-10.1.3 (AIAA 2008-8853)

DESIGN, FABRICATION AND OPERATION OF REMOTELY CONTROLLED AIRSHIPS IN INDIA

A. C. Gawale, A. A. Raina, R. S. Pant, et al

IIT, India

ICAS 2008-11.1 Terminal Operations: Chairs: J. Sorensen, Sensis, US; T. Davis, NASA, US

ICAS 2008-11.1.1 (AIAA 2008-8854)

TRAJECTORY UNCERTAINTY MODELING FOR QUEUEING ANALYSIS OF THE NATIONAL AIRSPACE SYSTEM

J. Kim, K. Palaniappan, P. K. Menon, et al

Optimal Synthesis Inc, USA

ICAS 2008-11.1.2 (AIAA 2008-8855)

MODELLING AIRLINE ROUTING AND SCHEDULING UNDER AIRPORT CAPACITY CONSTRAINTS

A. D. Evans, A. Schafer, L. Dray

Univ. of Cambridge, UK

ICAS 2008-11.1.3 (AIAA 2008-8856)

IMPROVING TERMINAL OPERATIONS - BENEFITS OF RNAV DEPARTURE PROCEDURES AT DALLAS-FORT WORTH AND HARTSFIELD-JACKSON ATLANTA INTERNATIONAL AIRPORTS

R. H. Mayer, K. P. Sprong

The MITRE Corporation, USA


 

Monday September 15th Afternoon Sessions

1330 - 1400

1400 - 1430

1430 - 1500

1500 - 1530

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

BREAK

 

 

 

 

 

 

 

 

 

 

 

 

1600 - 1630

1630 - 1700

1700 - 1730

1730 - 1800

ICAS 2008-1.2 Future Aircraft Concepts:

Chairs: C. Mathieu, ONERA, FR; I. Kroo, Stanford Univ., US

ICAS 2008-1.3 Design Methodology I:

Chairs: H. Mizuno, JAXA, JP; A. Pistek, Brno Univ. of Technology, CZ

ICAS 2008-1.2.1

CONCEPTUAL DESIGN OF A STOL REGIONAL-JET WITH HYBRID PROPULSION SYSTEM

C. Gologan

Bauhaus Luftfahrt e. V., Germany

ICAS 2008-1.2.2

DESIGN AND AERODYNAMIC ANALYSIS OF A LIGHT TWIN ENGINE PROPELLER AIRCRAFT

L. Pascale, F. Nicolosi*

Tecnam Aircraft Industries, Italy; *Second Univ. of Naples, Italy

ICAS 2008-1.2.3

CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION

Y. Tani, T. Yayama, J. -I. Hashimoto, et al

Kyushu Univ., Japan

ICAS 2008-1.2.4

AN ASSESSMENT OF THE POTENTIAL OF HYDROGEN FUELED LARGE LONG-RANGE TRANSPORT AIRCRAFT

D. Verstraete

Cranfield Univ., Belgium

ICAS 2008-1.3.1

AN APPROACH FOR MULTI-CRITERIA DECISION MAKING METHOD SELECTION AND DEVELOPMENT

Y. Li, N. Weston, D. Mavris

Georgia Institute of Technology, USA

ICAS 2008-1.3.2

A NEW SYSTEMS ANALYSIS: PERSPECTIVES ON SYSTEM-OF-SYSTEMS AND REGIONAL TRANSPORTATION PROOF-OF-CONCEPT STUDY

D. N. Fry, D. A. DeLaurentis

Purdue Univ., USA

ICAS 2008-1.3.3

PARAMETRIC SYSTEM EFFECTIVENESS ANALYSIS USING ARTIFICIAL NEURAL NETWORKS FOR BATTLE MANAGEMENT

P. T. Biltgen, D. N. Mavris

Georgia Institute of Technology, USA

ICAS 2008-1.3.4

LONG TERM AIRCRAFT PROJECT AND TECHNOLOGY EVALUATION UNDER THE UNCERTAINTY OF FUTURE SCENARIOS

M. Meussen, M. Trunk*, R. Henke**

AIRBUS S.A.S., France; *ARTS GmbH, France; **RWTH Aachen, Germany

ICAS 2008-2.2 High Lift:

Chairs: S, Ying, The Boeing Company, US; Y. Chen, First Aircraft Institute, CN

ICAS 2008-2.3 CFD Algorithms:

Chairs: C. Winkler, The Boeing Company, US

ICAS 2008-2.2.1

COMPUTATIONAL STUDY FOR HIGH-LIFT AERODYNAMICS RESEARCH IN JAXA

M. Murayama, Y. Yokokawa, H. Kato, et al

JAXA, Japan

ICAS 2008-2.2.2

NUMERICAL SIMULATION OF ICE ACCRETION ON MULTIPLE-ELEMENT AIRFOIL SECTIONS

S. J. Jacobs, J. M. Hospers, H. W. M. Hoeijmakers

Univ. of Twente, Netherlands

ICAS 2008-2.2.3

NUMERICAL AERODYNAMIC OPTIMISATIONS OF 3D HIGH-LIFT CONFIGURATIONS

J. Brezillon, R. P. Dwight, J. Wild

DLR, Germany

ICAS 2008-2.2.4

APPLICATION OF A NAVIER-STOKES CODE TO THE SIMULATIONS OF HIGH-LIFT DEVICES USING UNSTRUCTURED GRIDS

J. A. de Oliveira Neto, E. Basso, J. L. F. Azevedo*

CTA/IAE, Brazil; *CTA/IAE/ALA, Brazil

ICAS 2008-2.3.1

INTERFACE CONDITIONS OF FINITE-DIFFERENCE COMPACT SCHEMES FOR COMPUTATIONAL AEROACOUSTICS

T. Ikeda, T. Sumi, T. Kurotaki

JAXA, Japan

ICAS 2008-2.3.2

EULER INVERSE THROUGHFLOW MODEL BASED ON AN IMPLICIT UPWIND TIME MARCHING TECHNIQUE

S. Rosa Taddei, F. Larocca, F. Bertini*, et al

Politecnico di Torino, Italy; *Avio Group, Italy

ICAS 2008-2.3.3

THE APPLICATION OF ASEXUAL DNA ALGORITHM TO AIRFOIL DESIGN

L. Xia, Z. Gao, H. Zhan

NPU, China

ICAS 2008-2.3.4

AN AERODYNAMIC OPTIMIZATION FRAMEWORK BASED ON GENETIC ALGORITHMS

A. P. Antunes, R. G. da Silva, J. L. F. Azevedo*

Univ. of São Paulo, Brazil; *CTA/IAE/ALA, Brazil

ICAS 2008-3.2 Measurement Techniques:

Chairs: M. George, NASA, US; B. Rasuo, Univ. of Belgrade, Serbia

ICAS 2008-3.3 Vortex Control:

Chairs: S. Lieberg, The Boeing Company, US; F. Munteanu, INCAS, RO

ICAS 2008-3.2.1

DEVELOPMENT & APPLICATION OF MODERN MEASUREMENT TECHNIQUES FOR PRESSURIZED CRYOGENIC WIND TUNNELS

J. Quest, J. Leuckert*, U. Fey**, et al

ETW GmbH, Germany; *TU Berlin, Germany; **DLR, Germany

ICAS 2008-3.2.2

INVESTIGATION OF THE FLOW IN A RECTANGULAR CAVITY USING TOMOGRAPHIC AND TIME-RESOLVED PIV

C. Haigermoser, F. Scarano*, M. Onorato

Politecnico di Torino, Italy; *TU Delft, Netherlands

ICAS 2008-3.2.3

AEROACOUSTIC NOISE MEASUREMENTS IN AERODYNAMIC LOW-SPEED  WIND TUNNELS

T. Ito, H. Ura, Y. Yokokawa

JAXA, Japan

ICAS 2008-3.2.4

NUMERICAL STUDY OF A PITOT PROBE WITH FIVE-HOLE PYRAMIDAL HEAD FOR SUPERSONIC FLIGHT TEST

H. Ishikawa, D. Y. Kwak*, M. Noguchi*, et al

Sanko Soft Co.ltd, Japan; *JAXA, Japan

ICAS 2008-3.3.1 INVITED

THE SECOND INTERNATIONAL VORTEX FLOW EXPERIMENT (VFE-2): RESULTS OF THE FIRST PHASE 2003 - 2008

D. Hummel

TU Braunschweig, Germany

ICAS 2008-3.3.2

VORTEX BEHAVIORS OF CRANKED ARROW WING CONFIGURATIONS WITH DIFFERENT WING PLANFORMS

K. Hirai, D. Y. Kwak*, K. Rinoie

Univ. of Tokyo, Japan; *JAXA, Japan

ICAS 2008-3.3.3

INVESTIGATION OF THE FLOW OVER NACELLE/PYLON AND WING CONTROLLED WITH A VORTEX GENERATOR IN HIGH-LIFT CONFIGURATION

Y. Yokokawa, M. Kanazaki*, M. Murayama, et al

JAXA, Japan; *Tokyo Metropolitan Univ., Japan

ICAS 2008-3.3.4

FOREBODY VORTEX CONTROL ON HIGH PERFORMANCE AIRCRAFT USING PWM-CONTROLLED PLASMA ACTUATORS

T. Matsuno, H. Kawazoe, R. C. Nelson*, et al

Tottori Univ., Japan; *Univ. of Notre Dame, USA

ICAS 2008-4.2 Green Engine Concepts for the Future:

Chairs: N. Youssef, Pratt & Whitney Inc., CA; R. Kingcombe, DTI, UK

ICAS 2008-4.3 Combustion & Hypersonic:

Chairs: J. Hu, Pratt & Whitney Inc., CA

ICAS 2008-4.2.1

"ACTIVE CORE" - A KEY TECHNOLOGY FOR MORE ENVIRONMENTALLY FRIENDLY AERO ENGINES BEING INVESTIGATED UNDER THE NEWAC PROGRAM

S. Bock, W. Horn, J. Sieber

MTU Aero Engines GmbH, Germany

ICAS 2008-4.2.2

TOWARD ACARE 2020: INNOVATIVE ENGINE ARCHITECTURES TO ACHIEVE THE ENVIRONMENTAL GOALS?

S. Dron

Snecma, France

ICAS 2008-4.2.3

STUDIES ON MDO OF ENGINE DESIGN PARAMETERS WITH MISSION, NOISE & EMISSION CRITERIA AT SSBJ ENGINE CONCEPTUAL DESIGN

A. A. Mirzoyan

CIAM, Russian Federation

ICAS 2008-4.2.4

NEW METHOD TO ENHANCE THE WEARABILITY OF TITANIUM ALLOY ROTOR BLADE FOR AERO-ENGINE

J. S. Li, Y. M. Liang, J. Shi

Xi'an Aero-Engine (Group) Ltd., China

ICAS 2008-4.3.1

DEVELOPMENT OF AN INDUSTRIAL SCALE COMBUSTION TEST AND RESEARCH FACILITY FOR ALTERNATIVE FUELS AND FUEL FLEXIBILITY DEMONSTRATION

W. A. Chishty, I. Yimer, S. Manipurath, et al

NRC, Canada

ICAS 2008-4.3.2

DEVELOPMENT OF FULL ANNULAR COMBUSTOR FOR SMALL AIRCRAFT JET ENGINE IN JAXA TECHCLEAN PROJECT

M. Makida, H. Yamada, T. Yamamoto

JAXA, Japan

ICAS 2008-4.3.3

NUMERICAL STUDY OF ENERGY UTILIZATION IN NOZZLE/PLUME FLOW-FIELDS OF HIGH-SPEED AIR-BREATHING VEHICLES

D. Riggins, D. Moorhouse*, A. Wilson

Univ. of Missouri - Rolla, USA; *United States Air Force Research Laboratory, USA

ICAS 2008-4.3.4

FEASIBILITY STUDY ON MULTI-PHASE FLOW SIMULATION OF FUEL INJECTION USING LATTICE BOLTZMANN METHOD

A. Juhász, A. Veress, J. Rohács

Budapest Univ. of Technology and Economics, Hungary

ICAS 2008-5.2 Control Systems:

Chairs: Y. Miyazawa, Kyushu Univ., JP; M.-J. Tahk, KAIST, KR

ICAS 2008-5.3 Optimization:

Chairs: T. Tsuchiya, Univ. of Tokyo, JP; Z. Goraj, Warsaw Univ. of Technology, PL

ICAS 2008-5.2.1

AUTOMATIC FLIGHT CONTROL USING SAMPLED-DATA MIXED H_2/H_INFINITY OPTIMISATION

A.-M. Stoica, C. Dragasanu*

Univ. Politehnica of Bucharest & Romanian Space Agency, Romania; *Romanian Space Agency, Romania

ICAS 2008-5.2.2

ALLEVIATION OF ATMOSPHERIC FLOW DISTURBANCE EFFECTS ON AIRCRAFT RESPONSE

K. -U. Hahn, C. Schwarz

DLR, Germany

ICAS 2008-5.2.3

MECHANICALLY UNCOUPLED SERVO TABS FOR PRIMARY FLIGHT CONTROLS

Z. Khan

The Boeing Company, USA

ICAS 2008-5.2.4

RESEARCH ON CONTROL ALLOCATION FOR AIRCRAFTS WITH MULTIPLE CONTROL EFFECTORS

Y. Liu, Z. H Gao

NPU, China

ICAS 2008-5.3.1

AEROSPACE TRAJECTORY OPTIMIZATION: NOVEL VIEW ON A ROLE OF ATMOSPHERIC FLIGHT

A. S. Filatyev, A. A. Golikov

TsAGI, Russian Federation

ICAS 2008-5.3.2

UNIQUE PERFORMANCE CHARACTERISTICS OF SOLAR AIRCRAFT

G. Sachs, J. Lenz, F. Holzapfel

TU Munich, Germany

ICAS 2008-5.3.3

ON THE MINIMIZATION OF CRUISE DRAG DUE TO PITCH TRIM FOR A FLYING-WING CONFIGURATION

L. M. B. C. Campos, J. M. G. Marques*

IST & CCTAE, Portugal; *ULHT & CCTAE, Portugal

ICAS 2008-5.3.4

OPTIMIZATION FOR FLIGHT CONTROL SYSTEM WITH CONSTRAINTS SUPPLEMENTED HANDLING QUALITIES

Y. S. Kim, M. J. Tahk*

Hanwha Corp., Korea; *KAIST, Korea

ICAS 2008-6.2 Systems Design Methodology:

Chairs: W. Crossley, Purdue Univ., US;  D. Benchergui, Bombardier Aerospace, CA

ICAS 2008-6.3 Advances in Cabin Comfort:

Chairs: B. Stoufflet, Dassault Aviation, FR

ICAS 2008-6.2.1

A QUANTIFIED RELATIONSHIP MATRIX AIDED BY PROBABILISTIC DESIGN AND OPTIMIZATION

H. Gavel, J. Ölvander*, P. Krus*

Saab Aerosystems, Sweden; *Linköping Univ., Sweden

ICAS 2008-6.2.2

METHODOLOGY FOR AIRCRAFT SYSTEM ARCHITECTURE SIZING

C. de Tenorio, D. Mavris, E. Garcia, et al

Georgia Institute of Technology, USA

ICAS 2008-6.2.3

AN ADAPTABLE METHODOLOGY FOR AUTOMATION APPLICATION DEVELOPMENT

C. Van der Velden, C. Bil, X. Yu, et al

RMIT Univ., Australia

ICAS 2008-6.2.4

A SIMULATION FRAMEWORK FOR AIRCRAFT POWER SYSTEMS ARCHITECTING

S. Liscouët-Hanke

AIRBUS, France

ICAS 2008-6.3.1

INVESTIGATION OF LONG-HAUL FLIGHT ATTRIBUTES INFLUENCING PASSENGER'S BOOKING DECISION USING SP DATA

K. O. Ploetner

TU Munich, Germany

ICAS 2008-6.3.2

IMPACT OF CABIN PRESSURE ON ASPECTS OF THE WELL-BEING OF AIRCRAFT PASSENGERS – A LABORATORY STUDY

G. Grün, A. H. Holm, N. Luks*, et al

Fraunhofer Institute for Building Physics, Germany; *DLR, Germany

ICAS 2008-6.3.3

SCALING OF MIXED CONVECTION IN AIRCRAFT CABINS

A. Westhoff, J. Bosbach, C. Wagner

DLR, Germany

ICAS 2008-6.3.4

ICAS 2008-7.2 Composite Joints:

Chairs: T. Aoki, Univ. of Tokyo, JP; M.Scott, CRC-ACS, AUS

ICAS 2008-7.3 Composite Design I:

Chairs: W. Potkanski, Inst. of Aviation, PL; R. Dreisbach, The Boeing Company, US

ICAS 2008-7.2.1

INVESTIGATION OF ADHESIVELY BONDED COMPOSITE STRUCTURE JOINTS

N. Basso, M. Chrishti*, J. Bayandor*, et al

Politecnico di Milano, Italy; *RMIT Univ., Australia

ICAS 2008-7.2.2

LOADED CARBON COMPOSITE SCARF JOINTS SUBJECT TO QUASI STEADY LATERAL LOADS

H. C. H. Li, S. Feih, A. J. Gunnion*, et al

RMIT Univ., Australia; *CRC-ACS, Australia

ICAS 2008-7.2.3

THERMAL DESIGN UNDER UNCERTAINTIES OF AIRCRAFT STRUCTURES

J. Díaz, S. Hernández

Univ. of Coruna, Spain

ICAS 2008-7.2.4

MICROMECHANICAL FEM MODELING OF THERMAL STRESSES IN FUNCTIONALLY GRADED MATERIALS

S. Akbarpour, H. R. Motamedian, A. Abedian

Sharif Univ. of Technology, Iran

ICAS 2008-7.3.1

APPROXIMATIONS FOR FULLY ISOTROPIC  LAMINATE CONFIGURATIONS

C. B. York

Univ. of Glasgow, UK

ICAS 2008-7.3.2

THE DESIGN OF POSTBUCKLING COMPOSITE AEROSPACE STRUCTURES ACCOUNTING FOR DAMAGE INITIATION AND GROWTH

A. C. Orifici, R. S. Thomson*, R. Degenhardt**, et al

RMIT Univ., Australia; *CRC-ACS, Australia; **DLR, Germany

ICAS 2008-7.3.3

METAMODELS FOR THE OPTIMIZATION OF DAMAGE-TOLERANT COMPOSITE STRUCTURES

K. Kalnins, C. Bisagni*, R. Rikards, et al

Riga TU, Latvia; *Politecnico di Milano, Italy

ICAS 2008-7.3.4

CARBON/DYNEEMA INTRALAMINAR HYBRIDS: NEW STRATEGY TO INCREASE IMPACT RESISTANCE OR DECREASE MASS OF CARBON FIBER COMPOSITES

J. G. H. Bouwmeester, R. Marissen*, O. K. Bergsma**

DSM, NL; *DSM & TU Delft, NL; **TU Delft, NL

ICAS 2008-8.2 ATM I:

Chairs: J. Schroeder, NASA, US

 

ICAS 2008-8.3 Airport I:

Chairs: J. Stankunas, Antanas Gustaitis Aviation Institue, LT; B. Lamiscarre, ONERA, FR

ICAS 2008-8.2.1

CONTRACT-BASED AIR TRANSPORTATION SYSTEM TO FULFILL THE ARRIVING-ON-TIME OBJECTIVE

S. Guibert, L. Guichard, C. Rihacek*, et al

EUROCONTROL, France; *Frequentis AG, Austria

ICAS 2008-8.2.2

PREDICTION OF WEATHER-RELATED DELAYS IN THE CONTINENTAL UNITED STATES

B. Sridhar, D. Kulkarni

NASA, USA

ICAS 2008-8.2.3

RELATIONSHIP OF MAXIMUM MANAGEABLE AIR TRAFFIC CONTROL COMPLEXITY AND SECTOR CAPACITY

P. Kopardekar, J. Rhodes*, A. Schwartz*, et al

NASA, USA; *FAA, USA

ICAS 2008-8.2.4

HARMONIZING AUTOMATION, PILOT AND AIR TRAFFIC CONTROLLER IN THE FUTURE AIR TRAFFIC MANAGEMENT

E. Itoh, S. Suzuki*, V. Duong**

ENRI, Japan; *Univ. of Tokyo, Japan; **Eurocontrol Experimental Centre, France

ICAS 2008-8.3.1

AUGMENTED VISION VIDEOPANORAMA SYSTEM FOR REMOTE AIRPORT TOWER OPERATION

N. Fürstenau, M. Schmidt, M. Rudolph, et al

DLR, Germany

ICAS 2008-8.3.2

OPERATIONAL CONCEPT FOR AN AIRPORT OPERATIONS CENTER TO ENABLE TOTAL AIRPORT MANAGEMENT

G. Spies, F. Piekert, A. Marsden*, et al

DLR, Germany; *EUROCONTROL, France

ICAS 2008-8.3.3

AIRLINES’ POINT OF VIEW AS A NEW APPROACH TO MEASURING QUALITY OF SERVICE AT AIRPORTS

B. Badanik

Univ. of Zilina, Slovakia

ICAS 2008-8.3.4 (AIAA 2008-8965)

A METHODOLOGICAL APPROACH FOR AIRPORT TECHNOLOGY EVALUATION AND SELECTION

O. Pinon, E. Garcia, D. Mavris

Georgia Institute of Technology, USA

ICAS 2008-9.2 Human Factors:

Chairs: K. Leiden, Alion Science & Technology, US

ICAS 2008-9.3 Probabilistic Approaches Safety & Survivability:

Chairs: R. Paul, The Boeing Company, US

ICAS 2008-9.2.1

CBAQ: DEVELOPMENT OF CRM BEHAVIOR ANALYSIS METHOD FOR MISSION FLIGHT CREW TRAINING

T. Iijima, H. Tsuda, F. Noda

JAXA, Japan

ICAS 2008-9.2.2

AVIATION TELEMEDICINE: PAST, PRESENT AND FUTURE

J. S. Garrett, P. M. Alves

MedAire Inc., USA

ICAS 2008-9.2.3

IDENTIFYING FATIGUE OF FLIGHT ATTENDANTS IN SHORT-HAUL OPERATIONS

P. C. Shao, J -R. Yen, K. D. Ye

National Taiwan Ocean Univ., Taiwan

ICAS 2008-9.2.4

THE IMPLEMENTATION OF ANALYTICAL HIERARCHY PROCESS IN FLIGHT SAFETY

T. Wan, C. H. Hsieh*

Tamkang Univ., Taiwan; *ITRI, Taiwan

ICAS 2008-9.3.1

A PROGNOSTIC METHOD TO IDENTIFY HAZARDS FOR FUTURE AVIATION CONCEPTS

B. E. Smith, H. H. de Jong*, M. H. C. Everdij**

NASA, USA; *DFS, Germany; **NLR, Netherlands

ICAS 2008-9.3.2

A SIMULATION BENCHMARK FOR AIRCRAFT SURVIVABILITY ASSESSMENT

M. H. Smaili, J. Breeman, T. J. J. Lombaerts*, et al

NLR, Netherlands; *TU Delft, Netherlands

ICAS 2008-9.3.3

ADVANCED METHODOLOGIES FOR AVERAGE PROBABILITY CALCULATION FOR AEROSPACE SYSTEMS

A. Ramesh, D. Twig, T. Sharma

The Boeing Company, USA

ICAS 2008-9.3.4

FLIGHT SAFETY AS CONSIDERED IN PROBABILISTIC TERMS

J. L. Lewitowicz, G. Kowalczyk, K. Sibilski

Air Force Institute of Technology, Poland

ICAS 2008-10.2 Research to Reality (PANEL):

Chairs: P. Kopardekar, NASA, US

ICAS 2008-10.3 Impact of Economics on Production:

Chairs: P. Hollingsworth, Georgia Tech., US

ICAS 2008-10.2.1

ICAS 2008-10.2.2

ICAS 2008-10.2.3

ICAS 2008-10.2.4

ICAS 2008-10.3.1 (AIAA 2008-8861)

AUTOMATED ASSEMBLY TIME ANALYSIS USING A DIGITAL KNOWLEDGE BASED APPROACH

Y. Jin, R. Curran, J. Butterfield, et al

Queen's Univ. Belfast, Ireland

ICAS 2008-10.3.2 (AIAA 2008-8862)

USE OF DIGITAL MANUFACTURING TO IMPROVE MANAGEMENT LEARNING IN AEROSPACE ASSEMBLY

J. Butterfield, A. McClean, Y. Yin, et al

Queen's Univ. Belfast, Ireland

ICAS 2008-10.3.3 (AIAA 2008-8863)

INTERMITTENT DEMAND FORECAST BY COMBINING THE FORECASTS FROM SEVERAL METHODS INTO A COMPOSITE ONE WITHIN MRO SECTOR

A. Ghobbar

TU Delft, Netherlands

ICAS 2008-10.3.4 (AIAA 2008-8864)

DESIGN OF A LEAN MRO BUSINESS PROCESS FOR EPCOR

W. W. A. Beelaerts van Blokland, A. de Ward, S. C. Santema

TU Delft, Netherlands

ICAS 2008-11.2 Aircraft Performance:

Chairs: S. Brandt, US Air Force Academy, US; T.F. Morse, The Boeing Company, US

ICAS 2008-11.3 Operational Environmental Concerns:

Chairs: H. Pfaender, Georgia Tech., US

ICAS 2008-11.2.1 (AIAA 2008-8857)

SIMPLIFIED METHODS FOR ASSESSING THE IMPACT OF FUEL ENERGY CONTENT ON PAYLOAD-RANGE

T. M. Young

Univ. of Limerick, Ireland

ICAS 2008-11.2.2 (AIAA 2008-8858)

SIMULTANEOUS IMPROVEMENTS IN ENVIRONMENTAL PERFORMANCE AND OPERATIONAL EFFICIENCY ENABLED BY SIGNIFICANTLY QUIETER AIRCRAFT

J. Rachami, C. Morrow, B. Kim, et al

Wyle Laboratories, USA

ICAS 2008-11.2.3 (AIAA 2008-8859)

DEFINITION AND DEMONSTRATION OF THE AIRCRAFT PERFORMANCE EVALUATION CAPABILITIES (APECS) TOOL

S. Szurgyi

The MITRE Corporation, USA

ICAS 2008-11.2.4 (AIAA 2008-8860 )

USING AIRSPACEANALYZER TO EFFICIENTLY PROVIDE SPACING FOR AIRCRAFT ACROSS MULTIPLE SECTORS

W. P. Niedringhaus

The MITRE Corporation, USA

ICAS 2008-11.3.1 (AIAA 2008-8865)

ANALYSIS OF LATERAL FLIGHT INEFFICIENCY IN GLOBAL AIR TRAFFIC MANAGEMENT

T. G. Reynolds

Univ. of Cambridge, UK

ICAS 2008-11.3.2 (AIAA 2008-8866)

INTERDEPENDENCIES IN LOCAL AIR QUALITY AND NOISE IMPACTS FOR LANDING AND TAKEOFF OPERATIONS

S. Barret et al, I. Waitz*

Univ. of Cambridge, UK; *MIT, USA

ICAS 2008-11.3.3 (AIAA 2008-8867)

HIERARCHICAL AND SENSITIVITY ANALYSIS FOR NOISE ABATEMENT DEPARTURE PROCEDURES

X. Prats, J. Quevedo, V. Puig, et al

Technical Univ. of Catalonia, Spain

ICAS 2008-11.3.4 (AIAA 2008-8868)

TAILORED ARRIVALS OPERATIONS AT SFO AND EXPECTED ENVIRONMENTAL BENEFITS

K. R. Elmer, R. Mead, L. Bailey, et al

The Boeing Company, USA


 


Tuesday September 16th Morning Sessions

0800 - 0930                                                                                     GENERAL LECTURE I (INVITED) - Chairman: C. Mari, Messier-Bugatti, France

Prof. I. Waitz, MIT, USA: ENVIRONMENTAL IMPACT OF AVIATION: A REVIEW OF SELECTED US RESEARCH EFFORTS (ICAS 2008-0.2)

 Prof. D. Lee, Manchester Metropolitan Univ., UK: AVIATION CLIMATE IMPACT - A SUMMARY OF ONGOING EUROPEAN RESEARCH PROGRAMMES (ICAS 2008-0.3)

0930 - 1000                                                                                                                          BREAK

1000 - 1030

1030 - 1100

1100 - 1130

1130 - 1200

1200 - 1230

 

 

 

 

 

 

 

 

 

 

 

 

 

ICAS 2008-1.4 UAS Design I: Chairs: S. Ueno, Yokohama National Univ., JP; J. Fielding, Cranfield Univ., UK

ICAS 2008-1.4.1 INVITED

DESIGN OF NEXT GENERATION UNMANNED AIR SYSTEMS - ISSUES AND OPPORTUNITIES

M. S. Francis

General Atomics, USA

ICAS 2008-1.4.2

DESIGN AND DEVELOPMENT OF THE ECLIPSE AND DEMON DEMONSTRATOR UAVS

A. Yarf-Abbasi, A. Clarke, C. P. Lawson, et al

Cranfield Univ., UK

ICAS 2008-1.4.3

PRELIMINARY DESIGN OF A JOINED WING HALE UAV

D. Verstraete, M. Coatanéa, P. Hendrick

Université Libre de Bruxelles, Belgium

ICAS 2008-1.4.4

A NEW AIRCRAFT CONCEPT: THE COMBAT MALE

D. Manzato, F. Persiani, A. Beccaro*

Univ. of Bologna, Italy; *Alenia Aeronautica S.p.A, Italy

ICAS 2008-1.4.5

AUTONOMOUS AERIAL OBSERVATION SYSTEM FOR DISASTER RESPONSE USING ELECTRIC DUCTED FAN MAVS

N. Nagasaka, D. Kubo

Univ. of Tokyo, Japan

ICAS 2008-2.4 Supersonic Aerodynamics: Chairs: G. Eitelberg, DNW, NL, K. Bowcutt, The Boeing Company, US

ICAS 2008-2.4.1

LOW-BOOM AND LOW-DRAG OPTIMIZATION FOR THE TWIN-ENGINE SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR

T. Kumano, K. Sato, M. Yonezawa, et al

Tohoku Univ., Japan

ICAS 2008-2.4.2

FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1)

D. Y. Kwak, H. Ishikawa*, K. Yoshida

JAXA, Japan; *Sankou Soft Co. Ltd, Japan

ICAS 2008-2.4.3

WING DESIGN OF SUPERSONIC TRANSPORT BY A MULTI-POINT OPTIMIZATION METHOD

K. Higuchi, Z. Lei*, K. Rinoie

Univ. of Tokyo, Japan; *JAXA, Japan

ICAS 2008-2.4.4

AERODYNAMIC DESIGN OF THREE-DIMENSIONAL BIPLANE WINGS FOR LOW-WAVE DRAG SUPERSONIC FLIGHT

D. Maruyama

Tohoku Univ., Japan

ICAS 2008-2.4.5

COMPARISON OF SHOCK WAVE INTERACTION FOR THE THREE-DIMENSIONAL SUPERSONIC BIPLANE WITH DIFFERENT PLANAR SHAPES

M. Yonezawa, H. Yamashita

Tohoku Univ., Japan

ICAS 2008-3.4 Dynamic Testing: Chairs: K. Bathia, The Boeing Company, US; J. Nakamichi, JAXA, JP

ICAS 2008-3.4.1

FIN BUFFET CHARACTERISTICS OF ADVANCED TRAINER AIRCRAFT

C. Breitsamter, A. Schmid, J. U. Klar, et al

TU Munich, Germany

ICAS 2008-3.4.2

APPLICATION OF PVDF FOILS FOR THE MEASUREMENTS OF UNSTEADY PRESSURES ON WIND TUNNEL MODELS FOR THE PREDICTION OF AIRCRAFT VIBRATIONS

G. Luber, J. Becker (retired)

EADS-MAS, Germany

ICAS 2008-3.4.3

MEASUREMENT OF UNSTEADY AERODYNAMIC FORCES OF 3D FLAPPING WING IN HOVERING TO FORWARD FLIGHT

H. Nagai, K. Isogai*, T. Hayase**

Kyushu Inst. of Tech., Japan; *Nippon Bunri Univ., Japan; **Tohoku Univ., Japan

ICAS 2008-3.4.4

A SMALL SCALE PITCH-PLUNGE FLUTTER MODEL FOR ACTIVE FLUTTER CONTROL RESEARCH

A. N. Sutherland

Univ. of the Witwatersrand, South Africa

ICAS 2008-3.4.5

APPLICATION OF SEMICONDUCTOR STRAIN GAUGES IN MEASUREMENTS OF DYNAMIC STABILITY DERIVATIVES IN THE T-38 WIND TUNNEL

Z. Anastasijevic, M. Samardzic, D. Marinkovski

VTI, Serbia

ICAS 2008-4.4 Fans, Compressors, Aerodynamics and Aeromechanics: Chairs: A. Wadia, GE Aviation, US; F. Garnier, ONERA, FR

ICAS 2008-4.4.1

BIRD-STRIKE DAMAGE ANALYSIS IN CONCEPT ADVANCED COMPOSITE FAN BLADES

A. Zammit, M. Kim

RMIT Univ., Australia

ICAS 2008-4.4.2

INVESTIGATION OF SEPARATION CONTROL FOR LOW-PRESSURE TURBINES USING CFD

H. F. Fasel, W. Balzer, A. Gross

Univ. of Arizona, USA

ICAS 2008-4.4.3

NUMERICAL INVESTIGATION OF INLET DISTORTION INDUCED SWIRL IN MULTISTAGE FANS

A. Wadia, J. Yao*, S. Gorrell**

GE Aviation, USA; *GE Global Research, USA; **Air Force Research Lab, USA

ICAS 2008-4.4.4

NUMERICAL RESEARCHES ON THE AEROELASTIC PROBLEM OF TURBOMACHINERY

C. Zhang, Z. Ye*, F. Liu**

NPU, China; *National Key Laboratory of Aerodynamic Design and Research, China; **Univ. of California, USA

ICAS 2008-4.4.5

ICAS 2008-5.4 Handling Quality: Chairs: R. Katayanagi, Kanazawa Inst. of Technology, JP; F. Quagliotti, Politecnico di Torino, IT

ICAS 2008-5.4.1 INVITED

THEORETICAL APPROACH TO DIRECTIONAL CONTROL SENSITIVITY SELECTION

B. Lee, L. Zaichik*, V. Perebatov*, et al

The Boeing Company, USA; *TsAGI, Russian Federation

ICAS 2008-5.4.2

FEASIBILITY ANALYSIS OF ACHIEVING A STABILIZED APPROACH

M. M. Heiligers, T. van Holten, M. Mulder

TU Delft, Netherlands

ICAS 2008-5.4.3

CONTROLLABILITY OF BLENDED WING BODY AIRCRAFT

M. Voskuijl, G. La Rocca, F. Dircken

TU Delft, Netherlands

ICAS 2008-5.4.4

NEURAL NETWORK ANALYSIS OF PILOT MANEUVER DURING LANDING PHASE

R. Mori

Univ. of Tokyo, Japan

ICAS 2008-5.4.5

RESEARCH ON FUZZY LOGIC PIO DETECTOR

S. W. Yan, F. L. Tian*, Z. H. Gao, et al

NPU, China; *Chinese Flight Test Establishment, China

ICAS 2008-6.4 Subsystems & Equipments Improvements: Chairs: D. Blanding, The Boeing Company, US; R. Kingcombe, DTI, UK

ICAS 2008-6.4.1 INVITED

EVOLUTION OF FUTURE EQUIPMENTS AND SUB-SYSTEMS FOR THE FUTURE GREEN AIRCRAFT

J. Huysseune, O. Hiernaux

Thales Aerospace Division, France

ICAS 2008-6.4.2

MULTIVARIABLE CONTROLLER DESIGN FOR A TRIMMABLE HORIZONTAL STABILIZER ACTUATOR WITH TWO PRIMARY LOAD PATHS

N. Wachendorf, F. Thielecke, U. Carl, et al

TU Hamburg, Germany

ICAS 2008-6.4.3

MODELING OF ACOUSTICALLY TREATED NACELLE LIP TRANSPIRATION FLOW ANTI-ICING SYSTEM

R. Elangovan, R. F. Olsen, N. D. Reynolds

The Boeing Company, USA

ICAS 2008-6.4.4

SATELLITE-BASED NAVIGATION ARCHITECTURE STUDY FOR AIRCRAFT CATEGORY III LANDINGS

W. Schuster, J. Bai, W. Ochieng

Imperial College London, UK

ICAS 2008-6.4.5

A STUDY OF AN USER AND ENVIRONMENTAL FRIENDLY STORED ENERGY BASED EPU/APU-SYSTEM FOR MILITARY AEROSPACE APPLICATIONS

E. Prisell, J. Brandin*, O. Lyrsell**

FMV, Sweden; *Univ. of Lund, Sweden; **LUTAB, Sweden

ICAS 2008-7.4 Fatigue: Chairs: F. Abdi, Alpha STAR Corporation, US; T. Ueda, Nagoya University, JP

ICAS 2008-7.4.1

STATIC AND FATIGUE  ANALYSIS OF AN UPPER WING SKIN WITH EXFOLIATION CORROSION

G. Renaud, M. Liao, A. Uebersax*, et al

NRC, Canada; *RUAG Aerospace, Switzerland

ICAS 2008-7.4.2

FATIGUE ANALYSIS: THE SUPER-NEUBER TECHNIQUE FOR CORRECTION OF LINEAR ELASTIC FE RESULTS

L. Samuelsson

Volvo Aero AB, Sweden

ICAS 2008-7.4.3

FATIGUE DESIGN OF METALLIC COMPONENTS CONTAINING SURFACE OR INTERNAL DEFECTS

Y. Nadot, J. Mendez

ENSMA, France

ICAS 2008-7.4.4

FATIGUE BEHAVIOR AND LIFE PREDICTION OF WELDED TITANIUM ALLOY JOINTS

J. Liu, L. Wang, X.-R. Wu

BIAM, China

ICAS 2008-7.4.5

EFFECTS OF SUSPENSION WEIGHT ON FIGHTER FATIGUE DAMAGE

Z. Chen, Q. Zhu, J. Xue

BARC, China

ICAS 2008-8.4 Air Transport System: Chairs: C. Push, Eurocontrol, FR; Z. Goraj, Warsaw Univ. of Technology, PL

ICAS 2008-8.4.1

SYSTEM OF SYSTEMS DESIGN FOR WORLDWIDE COMMERCIAL AIRCRAFT NETWORKS

S. Shetty

The Boeing Company, USA

ICAS 2008-8.4.2

A HOLISTIC APPROACH TO EVALUATE THE AIR TRANSPORTATION SYSTEM

S. Langhans, V. Gollnick, E. Stumpf

DLR, Germany

ICAS 2008-8.4.3

IMPLEMENTING NEXT GENERATION AIR TRANSPORTATION SYSTEM TECHNOLOGIES

B. J. Holmes

DayJet Corporation, USA

ICAS 2008-8.4.4

PREDICTIVE MODELS OF THE NATIONAL AIRSPACE SYSTEM USING BAYESIAN NETWORKS

T. A. Lauderdale

NASA, USA

ICAS 2008-8.4.5

INNOVATIVE FUTURE AIR TRANSPORT SYSTEM: SIMULATION OF A FULLY AUTOMATED ATS

H. H. Toebben, C. Le Tallec*, A. Joulia*, et al

DLR, Germany; *ONERA, France

ICAS 2008-9.4 Crashworthiness and Impact: Chairs: M. Vellacott, Structural Monitoring Systems Ltd, AU; C. Kindervater, DLR, DE

ICAS 2008-9.4.1

IMPACT CHARACTERISTICS ESTIMATION OF SHORT SUPPORT COLUMNS UNDER CABIN FLOOR

H. Shoji, T. Aoki*

JAXA, Japan; *Univ. of Tokyo, Japan

ICAS 2008-9.4.2

A NEGATIVE SELECTION APPROACH TO DETECT DAMAGE IN AERONAUTICAL STRUCTURES WITH CHANGING OPERATING CONDITIONS

C. Surace, G. Surace, K. Worden*

Politecnico di Torino, Italy; *Univ. of Sheffield, UK

ICAS 2008-9.4.3

FE STUDY OF WINDSHIELD SUBJECTED TO HIGH SPEED BIRD IMPACT

M. Guida, A. Grimaldi, F. Marulo, et al

Univ. of Naples 'Federico II', Italy

ICAS 2008-9.4.4

BIRDSTRIKE ONTO STRUCTURES IN ROTATIONAL MOTION

L.-M. L. Castelletti, M. Anghileri

Politecnico di Milano, Italy

ICAS 2008-9.4.5 (AIAA 2008-8964 )

RECENT DEVELOPMENTS OF MSG-3 (MAINTANANCE STEERING GROUP) GUIDANCE FOR THE CONTINUED AIRWORTHINESS OF LIGHTNING/HIRF PROTECTION AND BENFITS TO NEW AIRPLANE DESIGN

G. J. Sweers, J. P. Fielding*

The Boeing Company, USA; *Cranfield Univ., UK

ICAS 2008-10.4 Impact of Economics on Operations: Chairs: E. Garcia, Georgia Tech., US

ICAS 2008-10.4.1 (AIAA 2008-8887)

TOWARD AN ECONOMIC MODEL TO INCENTIVIZE VOLUNTARY OPTIMIZATION OF NAS TRAFFIC FLOW

D. Littman, G. Hunter*

Synthesis Partners, USA; *Sensis Corporation, USA

ICAS 2008-10.4.2 (AIAA 2008-8888)

ANALYSIS OF INTERACTION BETWEEN AIR TRANSPORTATION AND ECONOMIC ACTIVITY

M. A. Ishutkina, R. J. Hansman

MIT, USA

ICAS 2008-10.4.3 (AIAA 2008-8889)

DEMAND-CENTRIC ANALYSIS OF THE AIR TRANSPORTATION SYSTEM

E. -S. Yang, J. -H. Lewe, D. N. Mavris

Georgia Institute of Technology, USA

ICAS 2008-10.4.4 (AIAA 2008-8890)

NETWORK AND ENVIRONMENTAL IMPACTS OF PASSENGER AND AIRLINE RESPONSE TO COST AND DELAY

L. M. Dray, A. Evans*, M. Vera-Morales, et al

Univ. of Cambridge, UK; * Univ. of Cambridge, UK

ICAS 2008-10.4.5 (AIAA 2008-8891)

EVALUATION OF ANCHORAGE INTERNATIONAL AIRPORT USING THE AIRPORT BUSINESS SUITE

P. C. Roling

TU Delft, Netherlands

ICAS 2008-11.4 Air Traffic Separation Assurance: Chairs: V. Schultz, NASA, US; R. Paielli, NASA, US

ICAS 2008-11.4.1 (AIAA 2008-8881)

SOME NEW POTENTIAL ASAS APPLICATIONS IN THE TERMINAL AND EN ROUTE DOMAINS

A. D. Mundra, D. A. Domino, A. P. Smith, et al

The MITRE Corporation, USA

ICAS 2008-11.4.2 (AIAA 2008-8882)

IMPACT OF PREDICTION UNCERTAINTY ON THE SAFETY PERFORMANCE OF AIRBORNE SEPARATION

M. Consiglio

NASA, USA

ICAS 2008-11.4.3 (AIAA 2008-8883)

A SYSTEM SAFETY FRAMEWORK FOR ANALYZING FUTURE AIR TRANSPORTATION SEPARATION ASSURANCE AND COLLISION AVOIDANCE CONCEPTS

S. J. Landry, A. V. Lagu

Purdue Univ., USA

ICAS 2008-11.4.4 (AIAA 2008-8884)

A PERFORMANCE ASSESSMENT OF A TACTICAL AIRBORNE SEPARATION ASSISTANCE SYSTEM USING REALISTIC, COMPLEX TRAFFIC FLOWS

J. C. Smith, F. J. L. Bussink*

NASA, USA; *National Institute of Aerospace, USA

ICAS 2008-11.4.5 (AIAA 2008-8885)

HUMAN-IN-THE-LOOP EVALUATION OF GROUND-BASED AUTOMATED SEPARATION ASSURANCE FOR NEXTGEN

T. Prevot, J. Homola, J. Mercer

San Jose State Univ./NASA Ames, USA

 


Tuesday September 16th Afternoon Sessions

 

1330 - 1415                                                                 GENERAL LECTURE II (INVITED) - Chairman: B. Laschka, Germany

                                                                                          Dr. J. Green, UK : ICAS - THE FIRST 50 YEARS (ICAS 2008-0.4)

 

   

1415 - 1430                                                                                                                    BREAK

1430 - 1500

1500 - 1530

1530 - 1600

 

 

 

 

 

 

 

 

 

 

 

 

 

1630 - 1700

1700 - 1730

1730 - 1800

1800 - 1830

ICAS 2008-1.5 UAS Design II:

Chairs: Y. Miyazawa; Kyushu Univ., JP

ICAS 2008-1.6 Conceptual Design Methods I:

Chairs: A. Kumar, NASA, US; G. Crouse, Auburn Univ., US

ICAS 2008-1.5.1

FLAPPING-WING TECHNOLOGY: THE POTENTIAL FOR AIR VEHICLE PROPULSION AND AIRBORNE POWER GENERATION

M. F. Platzer, J. Young*, J. C. S. Lai*

AeroHydro R&T Associates, USA; *Australian Defence Force Academy, Australia

ICAS 2008-1.5.2

MINI UAV DESIGN AND OPTIMIZATION FOR LONG ENDURANCE MISSION

Z. Goraj, J. Cisowski*, A. Frydrychewicz*, et al

WUT-IAAM, Poland; *WUT, Poland

ICAS 2008-1.5.3

DEVELOPMENT OF FLAPPING WING MICRO AIR VEHICLE

Y. F. Zhang, B. Song, Y. Z. Zhang

NPU, China

ICAS 2008-1.6.1

INNOVATIVE APPROACH FOR FUTURE AIRCRAFT DEVELOPMENT AT IAI

S. Tsach, O. Rix, B. Bublitsky

Israel Aerospace Industries, Israel

ICAS 2008-1.6.2

DEVELOPMENT AND VALIDATION OF A NEXT-GENERATION CONCEPTUAL AERO-STRUCTURAL SIZING SUITE

A. Bérard, L. Cavagna*, A. Da Ronch*, et al

KTH, Sweden; *Politecnico di Milano, Italy

ICAS 2008-1.6.3

CEASIOM: SIMULATING STABILITY & CONTROL WITH CFD/CSM IN AIRCRAFT CONCEPTUAL DESIGN

R. von Kaenel, A. Rizzi*, J. Oppelstrup*, et al

CFS, PSE-B, Switzerland; *KTH, Sweden

ICAS 2008-1.6.4

INCLUSION OF ENGINE RELATED PARAMETERS IN CONCEPTUAL DESIGN OF MORPHING AIRCRAFT

A. Sainadh, R. Pant

IIT Bombay, India

ICAS 2008-2.5 CFD Applications I:

Chairs: M. Mori, The Boeing Company, US; C. Atkin, City Univ. London, UK

ICAS 2008-2.6 CFD Applications II:

Chairs: T. Berglind, FOI, SE; D. Om, The Boeing Company, US

ICAS 2008-2.5.1

A CFD STUDY OF UCAV 1303 BASELINE MODEL AT CRUISE MACH NUMBERS

M. Khalid, W. Yuan, F. Zhang

NRC, Canada

ICAS 2008-2.5.2

EXPERIENCES OF GRID GENERATION AND STEADY/UNSTEADY VISCOUS COMPUTATIONS FOR COMPLEX GEOMETRIES

L. Tysell

FOI, Sweden

ICAS 2008-2.5.3

A TOOL FOR PARAMETRIC GEOMETRY AND GRID GENERATION FOR AIRCRAFT CONFIGURATIONS

G. L. Oliveira, L. C. C. Santos, A. L. Martins, et al

Embraer, Brazil

ICAS 2008-2.6.1

A LAYER PAVEMENT MODEL TO SIMULATE ROUGHNESS FEATURES IN ICE ACCRETION NUMERICAL SIMULATION

Y. Wang, D. W. Hammond*, G. P. Lin

BATRC/Beihang, China; *Cranfield Univ., UK

ICAS 2008-2.6.2

IHAAA STORE SEPARATION FROM CAVITY (SSC) PROJECT

E. Hallberg, L. Lijewski*, R. Deslandes**, et al

USNA, USA; *AFSEO, USA; **EADS, Germany

ICAS 2008-2.6.3

NUMERICAL SIMULATION OF VISCOUS FLOWS AROUND LIFTING BODIES OF COMPLICATED CONFIGURATION

A. Galaktionov, D. Fofonov

TSNIIMASH, Russian Federation

ICAS 2008-2.6.4

PREDICTION OF SUPERCOOLED DROPLET IMPINGEMENT ON HELICOPTER ROTOR BLADES

K. Szilder, H. Xu

NRC, Canada

ICAS 2008-3.5 Unconventional Flow Configurations:

Chairs: J. Rokicki, Warsaw Univ. of Technology, PL

ICAS 2008-3.6 Aerothermodynamics:

Chairs: B. Reinartz, RWTH Aachen, DE; K. Hatanaka, MHI, JP

ICAS 2008-3.5.1

AERODYNAMIC INVESTIGATIONS ON A GENERIC FAN-IN-WING CONFIGURATION

N. Thouault, C. Cologan*, C. Breitsamter, et al

TU Munich, Germany; *Bauhaus Luftfahrt, Germany

ICAS 2008-3.5.2

COMPUTATIONAL FLUID DYNAMICS AND EXPERIMENTAL INVESTIGATION OF AIRPLANE STALL DYNAMICS WITH WING CONTAMINATION

M. E. Beyers, M. Mamou, A. P. Brown, et al

NRC, Canada

ICAS 2008-3.5.3

NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE AERODYNAMICS OF UNCONVENTIONAL W-LEADING EDGE REVERSED DELTA WING IN GROUND EFFECT

M. Musaj, S. A. Prince

City Univ., UK

ICAS 2008-3.6.1

NUMERICAL ANALYSIS OF THIN-WALLED STRUCTURES IN HYPERSONIC FLOW REGIME

M. C. Haupt, R. Niesner, R. Unger, et al

TU Braunschweig, Germany

ICAS 2008-3.6.2

ANALYSIS OF THERMOCHEMICAL MODELING AND SURFACE  CATALYTICITY IN SPACE VEHICLE REENTRY

A. Viviani, G. Pezzella, C. Golia

Seconda Università di Napoli (SUN), Italy

ICAS 2008-3.6.3

NUMERICAL STUDY OF THE EFFECT OF THE OPPOSING JET ON REDUCTION OF AERODYNAMIC HEATING WITH DIFFERENT NOSE CONFIGURATIONS

I. Tamada, S. Aso, Y. Tani

Kyushu Univ., Japan

ICAS 2008-3.6.4

HEAT TRANSFER ON HYPERSONIC BLUNT BODIES WITH GAS INJECTION

V. V. Riabov

Rivier College, USA

ICAS 2008-4.5 Turbine Engine Operations:

Chairs: E. Prisell, FMV, SE

ICAS 2008-4.6 Turbine Engine Technology:

Chairs: C. Mari, Messier-Bugatti, FR

ICAS 2008-4.5.1

A FLIGHT THRUST DECK FOR THE F100 TURBOFAN OF THE F16 AIRCRAFT

P. Hendrick, K. Bourdiaudhy*, J. -F. Herbiet*

Université Libre de Bruxelles, Belgium; *Royal Military Academy of Belgium, Belgium

ICAS 2008-4.5.2

ON-CONDITION MAINTENANCE FOR NON-MODULAR JET ENGINES: AN EXPERIENCE

M. F. Siladic, B. Rasuo

Univ. of Belgrade, Serbia

ICAS 2008-4.5.3

AERODYNAMIC DESIGN AND ITS VALIDATION OF AN OPEN-TYPE ENGINE RUN-UP FACILITY

M. Kawai, K. Nagai, S. Aso*

IHI Corporation, Japan; *Kyushu Univ., Japan

ICAS 2008-4.6.1

PREPARING LP TURBINE TECHNOLOGY FOR MODERN AIRCRAFT ENGINES

J. Gier, N. Hübner, F. Kennepohl

MTU Aero Engines GmbH, Germany

ICAS 2008-4.6.2

EVALUATION OF THE FLOW IN AN INTERMEDIATE TURBINE DUCT AT OFF-DESIGN CONDITIONS

L.-U. Axelsson, T. G Johansson

Chalmers Univ. of Technology, Sweden

ICAS 2008-4.6.3

EXPERIMENTAL ANALYSIS OF THE FLOW FIELD IN A ROTATING 'U' CHANNEL

M. Gallo, T. Astarita, G. M. Carlomagno

DETEC - Univ. of Naples "Federico II", Italy

ICAS 2008-4.6.4

ICAS 2008-5.5 Flight Simulators:

Chairs: M. Yanagihara, JAXA, JP

ICAS 2008-5.6 UAS Control I:

Chairs: S. Levedag, DLR, DE; C. Bil, RMIT, AUS

ICAS 2008-5.5.1 INVITED

FLIGHT SIMULATORS – ON DIFFERENT PERCEPTIONS OF MANUFACTURERS, AVIATION AUTHORITIES, RESEARCH AND USERS

J.-M. Bauschat, J. Krüger*, D. Auger**

DLR, Germany; *Luftfahrt-Bundesamt (LBA), Germany; **CAE, Canada

ICAS 2008-5.5.2

RAVEN – A SUBSCALE RADIO CONTROLLED BUSINESS JET DEMONSTRATOR

D. Lundström, K. Amadori

Linköping Univ., Sweden

ICAS 2008-5.5.3

EXTENDING FMC TEST FOR FLIGHT SIMULATION AND FLIGHT EXPERIMENTS

Z. Li, H. Tang, S. Wang*

Chinese Flight Test Establishment, China; *NPU, China

ICAS 2008-5.6.1 (AIAA 2008-8962)

3D OBSTACLE AVOIDANCE STRATEGIES FOR UAS (UNINHABITED AERIAL SYSTEMS) MISSION PLANNING AND RE-PLANNING

F. De Crescenzio, G. Miranda, F. Persiani, et al

Univ. of Bologna, Italy

ICAS 2008-5.6.2

ROUTE PLANNING FOR RELAY UAV

A. Holmberg, P. -M. Olsson*

Saab Aerosystems, Sweden; *Linköping Univ., Sweden

ICAS 2008-5.6.3

TRAJECTORY OPTIMISATION FOR AUTONOMOUS VEHICLES: A MINIUAV APPLICATION

E. Capello, G. Guglieri, F. Quagliotti, et al

Politecnico di Torino, Italy

ICAS 2008-5.6.4

ANALYSIS OF DEEPSTALL LANDING FOR UAV

H. Taniguchi

Univ. of Tokyo, Japan

ICAS 2008-6.5 More Electric Aircraft I:

Chairs: C. Jaggard, Apptis corp., US; D. Benchergui, Bombardier Aerospace, CA

ICAS 2008-6.6 More Electric Aircraft II:

Chairs: D. Moorhouse, US Air Force Research Lab., US

ICAS 2008-6.5.1 INVITED

A VISION OF MORE ELECTRICAL AIRCRAFT AND CURRENT DEVELOPMENTS

J.-J. Charrier

Hispano-Suiza, France

ICAS 2008-6.5.2

A DUAL-OUTPUT POWER CONVERTER FOR LANDING GEAR ACTUATION USING MUTUAL POWER CIRCUIT COMPONENTS

T. Wijekoon, L. Empringham, P. W. Wheeler, et al

Univ. of Nottingham, UK

ICAS 2008-6.5.3

LATEST DEVELOPMENTS IN ELECTRIAL LANDING SYSTEMS

P. Monclar

Messier-Dowty, France

ICAS 2008-6.6.1

AUTOMATED GENERATION, SELECTION AND EVALUATION OF ARCHITECTURES FOR ELECTROMECHANICAL ACTUATORS

J. Liscouet, J.-C. Maré, S. Orieux

INSA/UPS, France

ICAS 2008-6.6.2

THERMAL MANAGEMENT OF ELECTROMECHANICAL ACTUATION ON AN ALL-ELECTRIC AIRCRAFT

C. P. Lawson, J. M. Pointon

Cranfield Univ., UK

ICAS 2008-6.6.3

EVAPORATING COOLANT FOR ON-BOARD COOLING SYSTEMS WITH DIRECT CONDENSATION THROUGH AMBIENT AIR

S. Adeyefa, F. Thielecke, U. Carl

TU Hamburg, Germany

ICAS 2008-6.6.4

A DUAL-DUPLEX ELECTROHYDRAULIC SYSTEM FOR THE FLY-BY-WIRE CONTROL OF A HELICOPTER MAIN ROTOR

G. Jacazio, P. Serena Guinzio, M. Sorli

Politecnico di Torino, Italy

ICAS 2008-7.5 Impact Damage:

Chairs: G. Guenther, EADS, DE

ICAS 2008-7.6 Crack Mechanisms:

Chairs: H. Abramovich, Technion, IL; A. de Boer, Univ. of Twente,NL

ICAS 2008-7.5.1

COHESIVE DISINTEGRATION IN IMPACTED RE-ENTRY SPACE TRANSPORTATION HYBRID STRUCTURES

J. Bayandor, F. Abdi*, B. Farahmand**

RMIT Univ., Australia; *Alpha Star Corporation, USA; **The Boeing Company, USA

ICAS 2008-7.5.2

COMPRESSION STRENGTH OF NOTCHED AND IMPACT DAMAGED COMPOSITE LAMINATES

M. Wallin, O. Saarela

Helsinki Univ. of Technology, Finland

ICAS 2008-7.5.3

PREDICTION OF DELAMINATION IN ADVANCED AEROSPACE COMPOSITE STRUCTURES USING MICRO/MACRO MECHANICS CONSTITUTIVE METHODS

S. Shah, J. Bayandor, F. Abdi, et al

RMIT Univ., Australia

ICAS 2008-7.6.1

FATIGUE CRACK GROWTH PREDICTION OF FIBRE REINFORCED METAL LAMINATES UNDER VARIABLE AMPLITUDE LOADING

S. U. Khan, R. C. Alderliesten, R. Benedictus

TU Delft, Netherlands

ICAS 2008-7.6.2

THE INFLUENCE OF FATIGUE CRACK INITIATION BEHAVIOUR OF FRICTION STIR WELDED JOINTS ON THE DESIGN CRITERIA

H. J. K. Lemmen, R. C. Alderliesten, J. J. Homan, et al

TU Delft, Netherlands

ICAS 2008-7.6.3

ESTIMATION OF CRACK TURN PHENOMENON

A. V. Berezin, A. V. Kulemin*, B. G. Nesterenko, et al

IMASH RAS, Russian Federation; *TsAGI, Russian Federation

ICAS 2008-7.6.4

ICAS 2008-8.5 Airport II:

Chairs: A. Boccanfuso, Transport Development Centre, CA

ICAS 2008-8.6 Operations:

Chairs: G. Fuentes, Avianca Airlines, CO

ICAS 2008-8.5.1

A PRACTICAL APPROACH TO MULTI-OBJECTIVE CAPACITY ANALYSIS OF AN ENVIRONMENT-AWARE AIRPORT

T. D. de Witte, R. H. Hogenhuis, M. J. A. van Eenige, et al

NLR, Netherlands

ICAS 2008-8.5.2

PRELIMINARY GUIDELINES ON FLIGHT DECK PROCEDURES FOR VERY CLOSELY SPACED PARALLEL APPROACHES

S. Verma, S. Lozito, G. Trot*

NASA, USA; *Raytheon Corp., USA

ICAS 2008-8.5.3

CAPACITY RESEARCH OF BRNO-TURANY AIRPORT WITH RESPECT TO NEW TRENDS IN AIR TRANSPORT

M. Stefanik, Z. Bazso

Univ. of Zilina, Slovakia

ICAS 2008-8.6.1

AN OPTIMIZATION MODEL FOR REDUCING AIRCRAFT TAXI TIMES AT THE DALLAS-FORT WORTH INTERNATIONAL AIRPORT

S. Rathinam, J. Montoya*, Y. Jung*

Univ. of California, USA; *NASA, USA

ICAS 2008-8.6.2

NOWCASTING THUNDERSTORM HAZARDS FOR FLIGHT OPERATIONS: THE CB WIMS APPROACH IN FLYSAFE

A. Tafferner, C. Forster, S. Sénési*, et al

DLR, Germany; *Météo-France, France

ICAS 2008-8.6.3

AN INTEGRATED USER-ORIENTED WEATHER FORECAST SYSTEM FOR AIR TRAFFIC USING REAL-TIME OBSERVATIONS AND MODEL DATA

C. Forster, A. Tafferner

DLR, Germany

ICAS 2008-8.6.4 (AIAA 2008-8977 )

BASE OF OPERATIONS CONCEPT FOR ON-DEMAND OPERATIONS

M. Mane, W. A. Crossley

Purdue Univ., USA

ICAS 2008-9.5 Structural Optimization:

Chairs: M. Wiedemann, DLR, DE

ICAS 2008-9.6 Aeroelasticity I:

Chairs: B. Nagel, DLR, DE; J. van Muijden, NLR, NL

ICAS 2008-9.5.1

STRUCTURAL MODEL TUNING CAPABILITY IN AN OBJECT-ORIENTED MULTIDISCIPLINARY DESIGN, ANALYSIS, AND OPTIMIZATION TOOL

S. -F. Lung, C. -G. Pak

NASA, USA

ICAS 2008-9.5.2

OPTIMALIZATION OF STIFFENED PANEL WITH THE HELP OF MATHEMATICAL PROGRAMMING - EXPERIMENTAL VERIFICATION

A. Pistek, M. Pesak

Brno Univ. of Technology, Czech Republic

ICAS 2008-9.5.3

OPTIMIZATION DESIGN ON PLATE-RIB STRUCTURE FOR CERTAIN KINDS OF AIRCRAFT

Y. C. Deng, C. Sun

Shenyang Aircraft Design and Research Institute, China

ICAS 2008-9.6.1 INVITED

ACTIVE AEROELASTICITY CONCEPT: NOVEL VIEW, METHODOLOGY AND RESULTS

G. Amiryants

TsAGI, Russian Federation

ICAS 2008-9.6.2

TRANSONIC FLUTTER WIND TUNNEL TESTS OF CONVENTIONAL TWIN-ENGINE TRANSPORT SEMISPAN MODEL

H. Arizono, K. Nakakita, J. Nakamichi

JAXA, Japan

ICAS 2008-9.6.3

DEVELOPMENT AND VALIDATION OF AN INVESTIGATION TOOL FOR NONLINEAR AEROELASTIC ANALYSIS

L. Cavagna, P. Masarati, S. Ricci, et al

Politecnico di Milano, Italy

ICAS 2008-9.6.4

DYNAMIC ANALYSIS OF AEROELASTIC RESPONSE FOR TRANSONIC FLOW WITH NONLINEAR STRUCTURAL MODEL

E. Camilo, F. D. Marques, J. L. F. Azevedo*

Univ. of São Paulo, Brazil; *Institute of Aeronautics and Space, Brazil

ICAS 2008-10.5 Pilot Simulation Studies:

Chairs: R. Shay, NASA, US; S. Engelland, NASA, US

 

ICAS 2008-10.6 Value Driven Design:

Chairs: R. Curran, Queen's Univ. Belfast, UK; P. Hollingsworth, Georgia Tech., US

ICAS 2008-10.5.1 (AIAA 2008-8895)

SAY WHO? PILOTED SIMULATION STUDY OF COMMUNICATIONS CENTERED AROUND A COCKPIT TRAFFIC DISPLAY

K. Kerns, R. Bone

The MITRE Corporation, USA

ICAS 2008-10.5.2 (AIAA 2008-8896)

PILOT IN-TRAIL PROCEDURE VALIDATION SIMULATION STUDY

F. J. L. Bussink, J. L. Murdoch*, J. P. Chamberlain*, et al

NIA, USA; *NASA, USA

ICAS 2008-10.5.3 (AIAA 2008-8897)

AN AUTOMATED SIMULATION PILOT CAPABILITY TO SUPPORT ADVANCED AIR TRAFFIC CONTROLLER TRAINING

R. Tarakan, N. Rozen, K. Baldwin

The MITRE Corporation, USA

ICAS 2008-10.6.1 (AIAA 2008-8903)

CONCURRENT AIRCRAFT DESIGN AND RESOURCE ALLOCATION UNDER UNCERTAINTY FOR ON-DEMAND AIR TRANSPORTATION

M. Mane, W. A. Crossley

Purdue Univ., USA

ICAS 2008-10.6.2 (AIAA 2008-8904)

AEROSPACE PRODUCT COST MANAGEMENT AT THE EARLY CONCEPT OPERATIONS PHASE

R. Curran, M. Gilmour, C. McAlleenen*, et al

Queens Univ., Belfast, UK; *Bombardier Aerospace, UK

ICAS 2008-10.6.3 (AIAA 2008-8905)

MULTI-OBJECTIVE AIRCRAFT OPTIMIZATION FOR MINIMUM COST AND EMISSIONS OVER SPECIFIC ROUTE NETWORKS

G. C. Bower, I. M. Kroo

Stanford Univ., USA

ICAS 2008-10.6.4 (AIAA 2008-8906 )

LIFE CYCLE ASSESSMENT OF ALUMINIUM FOR ENGINEERING APPLICATION

X. Tan, Y. Xu, J. Wang, et al

Queens Univ. Belfast, UK

ICAS 2008-11.5 Airspace Security:

Chairs: K. Tung Cate, NASA, US

ICAS 2008-11.6 Trajectory Prediction & Definition:

Chairs: S. Conway, The Boeing Company, US; J. Koelling, NASA, US

ICAS 2008-11.5.1 (AIAA 2008-8892)

AIRSPACE SECURITY MEASURES EMPLOYED FOR THE UN GENERAL ASSEMBLY MEETING: ANALYSIS AND IMPACT

P. Ostwald, D. Rowe, M. Howland

The MITRE Corporation, USA

ICAS 2008-11.5.2 (AIAA 2008-8893)

SECURE AIRSPACE: A CRITICAL COMPONENT OF NEXTGEN'S LAYERED, ADAPTIVE SECURITY

C. N. Bolczak, C. -C. V. Fong

The MITRE Corporation, USA

ICAS 2008-11.5.3 (AIAA 2008-8894)

SECURITY OF WIRELESS SENSOR NETWORK ENABLED HEALTH MONITORING FOR FUTURE AIRPLANES

R. Poovendran, K. Sampigethaya, L. Bushnell

Univ. of Washington, USA

ICAS 2008-11.6.1 (AIAA 2008-8898)

OPERATIONAL IMPROVEMENTS FROM IN-TRAIL PROCEDURE IN THE NORTH ATLANTIC ORGANIZED TRACK SYSTEM

R. C. Chartrand, F. J. L. Bussink*, T. J. Graff*, et al

NASA, USA; *NIA, USA

ICAS 2008-11.6.2 (AIAA 2008-8899)

MULTI-OBJECTIVE OPTIMIZATION OF USER PREFERRED 4D TRAJECTORIES IN THE NAS

I. Crook

ISA Software, Paris, France

ICAS 2008-11.6.3 (AIAA 2008-8900)

MODIFIED BEZIER CURVE FOR 4D REFERENCE TRAJECTORY DEFINITION UNDER FLIGHT PROFILE CONSTRAINT

T. Miquel, F. Mora-Camino*

DSNA, France; *CNRS, France

ICAS 2008-11.6.4 (AIAA 2008-8901)

FLIGHT DECK PROCEDURAL GUIDELINES FOR DATALINK TRAJECTORY NEGOTIATIONS

E. Mueller, S. Lozito

NASA, USA

 


Wednesday  September 17th Morning Sessions

0800 – 0900                                                          GENERAL LECTURE III (INVITED) - Chairman: J. Hefner, Past President ICAS, USA

                                                      Mr. A. Rauen, CEO Eurofighter GmbH , Germany: EUROFIGHTER/TYPHOON PROGRAMME (ICAS 2008-0.5)

 

 

0900 – 0930                                                                                                                              BREAK

0930 - 1000

1000 - 1030

1030 - 1100

1100 - 1130

1130 - 1200

 

 

 

 

 

 

 

 

 

 

 

 

 

ICAS 2008-1.7 Evolving Aircraft Concepts: Chairs: M. Drake, The Boeing Company, US; V. Gollnik, DLR, DE

ICAS 2008-1.7.1 INVITED

EVOLUTION OF EMBRAER’S CIVIL AIRCRAFT

H. B. Resende, D. H. Silva Filho, P. T. M. Lourencao

Embraer, Brazil

ICAS 2008-1.7.2

NACRE EUROPEAN PROJECT PROGRESS SUMMARY

J. Frota

AIRBUS, France

ICAS 2008-1.7.3

RE-INVENTING THE LEGEND:  THE DEVELOPMENT OF THE 747-8

C. Collisson

The Boeing Company, USA

ICAS 2008-1.7.4

AERODYNAMIC AND AERO-ACOUSTIC DESIGN OF MODERN TILT-ROTORS: THE ONERA EXPERIENCE

P. Beaumier, J. Decours, T. Lefebvre

ONERA, France

ICAS 2008-1.7.5

GRIPEN, PROGRAM OVERVIEW AND FUTURE DEVELOPMENT

H. Lindell

Saab Aerosystems, Sweden

ICAS 2008-2.7 Flow Control I: Chairs: G. Lombardi, University of Pisa, IT; H. Consigny, ONERA, FR

ICAS 2008-2.7.1

CONTROL OF A SWEPT WING TAILLESS AIRCRAFT THROUGH  WING MORPHING

R. W. Guiler, W. W. Huebsch*

Aurora Flight Sciences, USA; *West Virginia Univ., USA

ICAS 2008-2.7.2 INVITED

AERODYNAMIC DESIGN OF THE  A400M HIGH-LIFT SYSTEM

D. Reckzeh

AIRBUS, Germany

ICAS 2008-2.7.3

SINGLE VERSUS MULTIPLE WINGLETS: NUMERICAL AND EXPERIMENTAL INVESTIGATION

D. P. Coiro, F. Nicolosi, F. Scherillo, et al

Univ. of Naples "Federico II", Italy

ICAS 2008-2.7.4

COMPUTATIONS FOR LAMINAR FLOW CONTROL IN SWEPT-WING BOUNDARY LAYERS

H. L. Reed, R. G. Rhodes, W. S. Saric

Texas A and M Univ., USA

ICAS 2008-2.7.5

FLIGHT EXPERIMENTS ON SWEPT WING TRANSITION USING DISTRIBUTED ROUGHNESS

W. S. Saric, A. L. Carpenter, H. L. Reed

Texas A and M Univ., USA

ICAS 2008-3.7 Surface Flows: Chairs: D. Knoerzer, European Commission, BE; C. Breitsamter, TU Munich, DE

ICAS 2008-3.7.1

A WALL SHEAR STRESS MEASUREMENT TECHNIQUE USING THE THERMAL WAKES OF SMALL HEATED SPOTS

I. Rudolph, M. Reyer, W. Nitsche

TU Berlin, Germany

ICAS 2008-3.7.2

PERFORMANCE DEGRADATION OF A SIMULATED ICE CONTAMINATED AIRFOIL BY SUPER-COOLED DROPLETS

Z. Patek, L. Smrcek*, R. A . McD. Galbraith*

VZLU, Czech Republic; *Univ. of Glasgow, UK

ICAS 2008-3.7.3

IN-FLIGHT EXPERIMENTS FOR DELAYING LAMINAR-TURBULENT TRANSITION ON A LAMINAR WING GLOVE

I. Peltzer, A. Pätzold, W. Nitsche

TU Berlin, Germany

ICAS 2008-3.7.4

PIV FLOW MEASUREMENTS FOR A HIGH LIFT AIRFOIL WITH LEADING EDGE ICE

J. H. M. Gooden

NLR, Netherlands

ICAS 2008-3.7.5

EXPERIMENTAL STUDY ON INTERFERENCE FLOW OF A SUPERSONIC BUSEMANN BIPLANE USING PRESSURE-SENSITIVE PAINT TECHNIQUE

H. Nagai, S. Oyama, T. Ogawa, et al

Tohoku Univ., Japan

ICAS 2008-4.7 Environmental Challenges: Chairs: C. Hellstrand, The Boeing Company, US

ICAS 2008-4.7.1 INVITED

AIRBUS: TOWARDS AN ECO-EFFICIENT ENTERPRISE

M. Goulain

Airbus, France

ICAS 2008-4.7.2

GOING GREEN – MITIGATING AVIATION’S NEW ENVIRONMENTAL DRIVERS

N. Brown, C. Burleson, C. Holsclaw, et al

FAA, USA

ICAS 2008-4.7.3

THE ENVIRONMENTAL DESIGN SPACE

M. R. Kirby, D. N. Mavris

Georgia Institute of Technology, USA

ICAS 2008-4.7.4

PAYLOAD FUEL ENERGY EFFICIENCY AS A METRIC FOR AVIATION ENVIRONMENTAL PERFORMANCE

J. I. Hileman, J. B. Katz, J. G. Mantilla*, et al

MIT, USA; *John A. Volpe National Transportation Systems Center, USA

ICAS 2008-4.7.5

THE FEASIBILITY AND POTENTIAL ENVIRONMENTAL BENEFITS OF ALTERNATIVE FUELS FOR COMMERCIAL AVIATION

J. I. Hileman, H. M. Wong, D. Ortiz*, et al

MIT, USA; *Rand Corp., USA

ICAS 2008-5.7 Guidance: Chairs: J.P. Jung, ONERA, FR

ICAS 2008-5.7.1 INVITED

IMPROVEMENT FOR LANDING ON SMALL-MEDIUM AIRPORTS USING FUTURE, AIRCRAFT-AUTONOMOUS GUIDANCE AIDS

G. Sachs, F. Schuck, F. Holzapfel, et al

TU Munich, Germany

ICAS 2008-5.7.2

TRAJECTORY CONTROL IMPROVEMENT BASED ON A NONLINEAR DYNAMIC INVERSION APPROACH

L. Höcht, F. Holzapfel, G. Sachs

TU Munich, Germany

ICAS 2008-5.7.3

INTEGRATED INTERCEPT MISSILE GUIDANCE AND CONTROL WITH TERMINAL ANGLE CONSTRAINT

H. S. Shin, T. W. Hwang*, A. Tsourdos**, et al

KAIST, Korea; *Agency for Defence Development, Korea; **Cranfield Univ., UK

ICAS 2008-5.7.4

NONLINEAR FORMATION GUIDANCE LAW WITH ROBUST DISTURBANCE OBSERVER

H. S. Shin, T. H Kim, T. W Hwang*, et al

KAIST, Korea; *ADD, Korea

ICAS 2008-5.7.5

TRAJECTORY DESIGN OF SILENT SUPERSONIC TECHNOLOGY DEMONSTRATOR (S3TD)

H. Suzuki

JAXA, Japan

ICAS 2008-6.7 Lean Engineering and Development: Chairs: E. Murman, MIT, US; R. Bengelink, Arizona State Univ., US

ICAS 2008-6.7.1

LEAN PRODUCT DEVELOPMENT IN THE AEROSPACE ENTERPRISE

E. Rebentisch

MIT, USA

ICAS 2008-6.7.2

F/A 18 E/F TOTAL PRODUCTION SYSTEM

K.W. Katzenberger

The Boeing Company, USA

ICAS 2008-6.7.3

USING LEAN PRINCIPLES AND MBE IN DESIGN AND DEVELOPMENT OF AVIONICS EQUIPMENT AT ROCKWELL COLLINS

D. Lempia

Rockwell Collins Inc., USA

ICAS 2008-6.7.4

DESIGN FOR PROCESS EXCELLENCE - ENSURING TIMELY AND COST EFFECTIVE SOLUTIONS

N. Egbert, P. McCoy, D. Schwerin, et al

Rolls Royce Corp., USA

ICAS 2008-6.7.5

APPLICATION OF THE INTEGRATED PRODUCT TEAM (IPT) CONCEPT TO THE RE-ENGINE OF A VERY LIGHT JET (VLJ)

M. S. Attia, C. L. Cassano, R. C. Schmidt

Embry-Riddle Univ., USA

ICAS 2008-7.7 Aeroelasticity II: Chairs: J. Hoffren, Helsinki Univ. of Technology, FI; W.D. Anderson, Lockheed Martin, US

ICAS 2008-7.7.1

EFFICIENT AEROELASTIC SIMULATION IN A PARAMETRIC PROCEDURE FOR FATIGUE ANALYSIS

J. van Muijden, B. B. Prananta, R. P. G. Veul

NLR, Netherlands

ICAS 2008-7.7.2

MONITORING OF OSCILLATORY FAILURE CASES FOR THE REDUCTION OF STRUCTURAL LOADS IN AN AEROELASTIC AIRCRAFT

H. Sachs, U. B. Carl, F. Thielecke

TU Hamburg, Germany

ICAS 2008-7.7.3

UNIFIED BE-FE AERODYNAMIC-ACOUSTIC-STRUCTURE COUPLING SCHEME FOR ACOUSTIC EFFECTS ON AEROELASTIC STRUCTURES

H. Djojodihardjo

Universitas Al-Azhar (Indonesia) & Universiti Sains, Malaysia

ICAS 2008-7.7.4

UNSTEADY AERO-ELASTIC COUPLING FOR THE F/A-18 VERTICAL TAIL BUFFETING

M. Guillaume, J. Vos*, A. Gehri, et al

RUAG Aerospace, Switzerland; *CFS Engineering, Switzerland

ICAS 2008-7.7.5

SCALED DOWN MODELS FOR FREE VIBRATION ANALYSIS OF ORTHOGONALLY STIFFENED CYLINDRICAL SHELLS USING SIMILITUDE THEORY

S. Torkamani, A. A. Jafari, H. M. Navazi*

K.N. Toosi Univ. of Technology, Iran; *Sharif Univ. of Technology, Iran

ICAS 2008-8.7 Aircraft Separation: Chairs: M. Peters, NLR, NL; T. Goetzendorf-Grabowski, Warsaw University of Technology, PL

ICAS 2008-8.7.1

PERFORMANCE BASIS FOR AIRBORNE SEPARATION

D. J. Wing

NASA, USA

ICAS 2008-8.7.2

ASSESSMENT OF FLIGHT CREW ACCEPTANCE OF AUTOMATED RESOLUTION SUGGESTIONS AND MANUAL RESOLUTION TOOLS

V. Battiste, W. J. Johnson*, A. Q. Dao, et al

San Jose State Univ., USA; *NASA, USA

ICAS 2008-8.7.3

REAL-TIME SIMULATION OF A DISTRIBUTED CONFLICT RESOLUTION ALGORITHM

G. T. Spence, D. J. Allerton, R. Baumeister*, et al

Univ. of Sheffield, UK; *The Boeing Company, USA

ICAS 2008-8.7.4

A SYSTEMATIC PROCEDURE FOR DETERMINING  SEPARATION MINIMA

Y. J. Zhao

Univ. of Minnesota, USA

ICAS 2008-8.7.5

ALGORITHM AND OPERATIONAL CONCEPT FOR RESOLVING SHORT-RANGE CONFLICTS

H. Erzberger, K. Heere,

Univ. of California, USA

ICAS 2008-9.7 ATM Safety Assessments: Chairs: R. Coppenbarger, NASA, US

ICAS 2008-9.7.1

THE IMPACT OF RIGOROUS METHODS ON AERONAUTICAL REGULATIONS

E. R. Lopez Ruiz, M. Lemoine

ONERA, France

ICAS 2008-9.7.2

HAZARD, SAFETY RISK AND UNCERTAINTY MODELING OF THE INTEGRATION OF UNMANNED AIRCRAFT SYSTEMS INTO THE NATIONAL AIRSPACE

A. Oztekin, J. T. Luxhoj

Rutgers Univ., USA

ICAS 2008-9.7.3

THE SAFETY GAINED BY EQUIPMENT AND PROCEDURES USED TO PERFORM CONSTANT ANGLE APPROACHES

D. Carbaugh

The Boeing Company, USA

ICAS 2008-9.7.4

COMPARING SITUATION AWARENESS MEASUREMENT TECHNIQUES IN A LOW FIDELITY AIR TRAFFIC CONTROL SIMULATION

R. S. Pierce, T. Z. Strybel*, K. -P. L. Vu*

Univ. of California, Riverside, USA; *California State Univ., LB, USA

ICAS 2008-9.7.5

A MODEL FOR ESTIMATING THE LATERAL OVERLAP PROBABILITY OF AIRCRAFT WITH RNP ALERTING CAPABILITY IN PARALLEL RNAV ROUTES

S. Nagaoka

ENRI, Japan

ICAS 2008-10.7 Weather Considerations: Chairs: J. Murphy, NASA, US

ICAS 2008-10.7.1 (AIAA 2008-8914)

CAUSALITY ANALYSIS FOR AVIATION WEATHER HAZARDS

J. Krozel, W. M. McNichols, J. Prete, et al

Metron Aviation, USA

ICAS 2008-10.7.2 (AIAA 2008-8915)

AN ATMOSPHERIC SIMULATION SYSTEM FOR AVIATION REQUIREMENTS OVER NORTHERN LATITUDES

A. Sarma

SAIC, USA

ICAS 2008-10.7.3 (AIAA 2008-8916)

ESTIMATION OF AIR TRAFFIC DELAY USING THREE DIMENSIONAL WEATHER INFORMATION

N. Y. Chen, B. Sridar*

Univ. of California Santa Cruz, USA; *NASA, USA

ICAS 2008-10.7.4 (AIAA 2008-8917)

METHODOLOGIES FOR ESTIMATING THE IMPACT OF SEVERE WEATHER ON AIRSPACE CAPACITY

L. Song, C. Wanke, D. Greenbaum, et al

The MITRE Corporation, USA

ICAS 2008-10.7.5 (AIAA 2008-8918)

OPERATIONAL ASSESSMENT OF THE INTEGRATED TERMINAL WEATHER SYSTEM (ITWS) USING DIRECT MEASUREMENT

D. Howell, G. Paull, J. Sunderlin

MCR Federal, USA

ICAS 2008-11.7 Traffic Flow Management I: Chairs: R. Eveleigh, Eurocontrol, FR; B. Windhorst, NASA, US

ICAS 2008-11.7.1 (AIAA 2008-8907)

MODEL-BASED AIR TRAFFIC FLOW MANAGEMENT

P. K. Menon, M. D. Tandale, J. S. Kwan, et al

Optimal Synthesis Inc, USA

ICAS 2008-11.7.2 (AIAA 2008-8908)

AN ESTIMATION OF THE BENEFITS OF AIR TRAFFIC FLOW MANAGEMENT

J. DeArmon, J. Hoffman, T. Holden, et al

The MITRE Corporation, USA

ICAS 2008-11.7.3 (AIAA 2008-8909)

TASK ANALYSIS FOR FEASIBILITY ASSESSMENT OF A COLLABORATIVE TRAFFIC FLOW MANAGEMENT CONCEPT

J. L. Garcia-Chico, H. Idris, J. Krozel*, et al

L-3 Communications, USA; *Metron Aviation Inc, USA

ICAS 2008-11.7.4 (AIAA 2008-8910)

SOLVING HIGH-FIDELITY, LARGE-SCALE TRAFFIC FLOW MANAGEMENT PROBLEMS IN REDUCED TIME

J. Rios, K. Ross*

NASA, USA; *Univ. of California at Santa Cruz, USA

ICAS 2008-11.7.5 (AIAA 2008-8911)

COLLABORATIVE FLOW MANAGEMENT: ANALYSIS OF BENEFITS DURING CONVECTIVE WEATHER DISRUPTIONS

M. Berge et al

The Boeing Company, USA

 

 

Wednesday September 17th Afternoon Sessions

1330 - 1415                                       ICAS JOHN SWIHART LECTURE FOR INNOVATION IN AERONAUTICS (INVITED) - Chairman: D. Müller-Wiesner, EADS, Germany

                                                       Prof. A. Starik, CIAM, Russia: INNOVATIONS IN COMBUSTION TECHNOLOGY FOR PROPULSION (ICAS 2008-0.6)

1430 - 1500

1500 - 1530

1530 - 1600

 

 

 

 

 

 

 

 

 

 

 

 

 

1630 - 1700

1700 - 1730

1730 - 1800

1800 - 1830

ICAS 2008-1.8 Conceptual Design Methods II:

Chairs: C. Svoboda, The Boeing Company, US

ICAS 2008-1.9 Aircraft Design and Optimization:

Chairs: M. Price, Queen's Univ. Belfast, UK; D. Carter, Air Force Research Lab., US

ICAS 2008-1.8.1

AIRCRAFT CONCEPTUAL DESIGN AUTOMATION

K. Amadori, C. Jouannet, P. Krus

Linköping Univ., Sweden

ICAS 2008-1.8.2

COMPUTATIONAL TOOLS FOR AIRCRAFT SYSTEM ANALYSIS AND OPTIMIZATION

P. Krus

Linköping Univ., Sweden

ICAS 2008-1.8.3

UNCERTAINTY QUANTIFICATION FOR CAPABILITY-BASED SYSTEMS-OF-SYSTEMS DESIGN

P. T. Biltgen

Georgia Institute of Technology, USA

ICAS 2008-1.9.1 (AIAA 2008-8926)

A SYSTEMATIC APPROACH IN AIRCRAFT CONFIGURATION DESIGN OPTIMIZATION

M. Sadraey

Daniel Webster College, USA

ICAS 2008-1.9.2 (AIAA 2008-8927)

DOMAIN SPECIFIC MODELING LANGUAGES TO SUPPORT MODEL-DRIVEN ENGINEERING OF AIRCRAFT SYSTEMS

S. W. G. van der Elst, M. J. L. van Tooren

TU Delft, Netherlands

ICAS 2008-1.9.3 (AIAA 2008-8928)

FUNCTION BASED ARCHITECTURE DESIGN SPACE DEFINITION AND EXPLORATION

M. Armstrong, C. De Tenorio, E Garcia, et al

Georgia Institute of Technology, USA

ICAS 2008-1.9.4 (AIAA 2008-8929)

ADVANCED GENERAL AVIATION DESIGN WITH TRANSPORTATION ARCHITECTURE ANALYSIS

H. T. Won, J. -H. Lewe, D. N. Mavris

Georgia Institute of Technology, USA

ICAS 2008-2.8 Aerodynamic Optimisation I:

Chairs: A. Dillmann, DLR, DE; W. J. McCroskey, US Army (ret.), US

ICAS 2008-2.9 Store Separation:

Chairs: C. Winkler, The Boeing Company, US; B. Whiting, The Boeing Company, US

ICAS 2008-2.8.1

TOWARDS AERODYNAMIC OPTIMISATION OF AN AEROELASTIC WING USING DOMAIN ELEMENT PARAMETERISATION

A. M. Morris, C. B. Allen, T. C. S. Rendall

Univ. of Bristol, UK

ICAS 2008-2.8.2

APPLICATION OF AN HYBRID OPTIMIZATION APPROACH IN THE DESIGN OF LONG ENDURANCE AIRFOILS

M. S. Khurana

RMIT Univ., Australia

ICAS 2008-2.8.3

ON AIRCRAFT PERFORMANCE IMPROVEMENT BY USING WINGLETS

B. Rasuo, V. Parezanovic, M. Adzic

Univ. of Belgrade, Serbia

ICAS 2008-2.9.1

TRANSONIC STORE SEPARATION STUDIES ON THE SAAB GRIPEN AIRCRAFT USING COMPUTATIONAL AERODYNAMICS

I. Persson, A. Lindberg

Saab Aerosystems, Sweden

ICAS 2008-2.9.2

TARGETING PODS EFFECTS ON STORE SEPARATION CHARACTERISTICS: A JOINT NRC-IAR/USNAVY CFD EFFORT

A. Benmeddour, F. Fortin, Y. Mébarki, et al

National Research Council, Canada

ICAS 2008-2.9.3

STORE SEPARATION TRAJECTORY SIMULATION FOR THE HIGH SPEED ANTI-RADIATION DEMONSTRATOR (HSAD) FROM THE F-4 AIRCRAFT

E. N. Hallberg, A. Cenko*, S. Dodbelle*

United States Naval Academy, USA; *Naval Air Systems Command, USA

ICAS 2008-2.9.4

TARGETING POD EFFECTS ON WEAPONS RELEASE FROM THE F-18C HORNET

W. H. Godiksen III, E. N. Hallberg

United States Naval Academy, USA

ICAS 2008-3.8 Boundary Layers:

Chairs: W. Nitsche, TU Berlin, DE

ICAS 2008-3.9 Unsteady Flow I:

Chairs: H. Resende, Embraer, BR; C. Breitsamter, TU Munich, DE

ICAS 2008-3.8.1

THE EFFECTS OF WALL ROUGHNESS ON THE TURBULENT BOUNDARY LAYER        

L. Vesely, C. Haigermoser, M. Onorato

Politecnico di Torino, Italy

ICAS 2008-3.8.2

WHITE LIGHT SKIN-FRICTION AND GAS DENSITY MEASUREMENTS AROUND A SUPERSONIC FOREBODY

J. M. Desse, P. d'Espiney

ONERA, France

ICAS 2008-3.8.3

LAMINAR-TURBULENT TRANSITION CORRELATION IN SUPERSONIC/ HYPERSONIC FLOW – ATTACHED VERSUS SEPARATED FLOW

G. A. Simeonides

Hellenic Aerospace Industry, Greece

ICAS 2008-3.9.1

VORTEX WAKE INVESTIGATION BEHIND A WING-FLAP MODEL WITH JET SIMULATION

L. L. M. Veldhuis, R. de Kat

TU Delft, Netherlands

ICAS 2008-3.9.2

VORTEX BLOB METHOD AS VISUALIZATION TOOL FOR MULTI-ELEMENT AIRFOIL FLOWS OPTIMIZATION

C. Golia, B. Buonomo

Second Univ. of Naples, Italy

ICAS 2008-3.9.3

UNSTEADY PROPULSIVE CHARACTERISTICS OF BIOFOILS MOVING IN A VERY LOW-REYNOLDS NUMBER FLOW

C. H. Han, S. J. An*, J. S. Maeng*

Chungju National Univ., Korea; *Hanyang Univ., Korea

ICAS 2008-3.9.4

ON THE EFFECTS ON NOISE OF GROUND REFLECTION AND ATMOSPHERIC ATTENUATION ON THE NOISE OF HELICOPTERS

L. M. B. C. Campos, J. M. G. S. Oliveira

IST, Portugal

ICAS 2008-4.8 Reducing Approach and Climb-Out Noise:

Chairs: D. Arbuckle, NextGen JPDO (NASA), US

ICAS 2008-4.9 Internal Noise:

Chairs: F. Haselbach, Rolls-Royce, UK; A. de Boer, Univ. of Twente,NL

ICAS 2008-4.8.1

EVALUATION OF SIMULATOR AND FLIGHT TESTED NOISE ABATEMENT APPROACH PROCEDURES

R. Koenig, O. Macke

DLR, Germany

ICAS 2008-4.8.2

DESIGN OF 4D LANDING APPROACH TRAJECTORIES FOR A QUIET STOL AIRPLANE

O. Macke, R. Koenig

DLR, Germany

ICAS 2008-4.8.3

NOISE REDUCTION BY THRUST VECTORING FOR SUPERSONIC BUSINESS JET

S. Horinouchi

JAXA, Japan

ICAS 2008-4.9.1 INVITED

ENVIRONMENTALLY PROGRESSIVE AIRPLANES THROUGH AN INTEGRATED DESIGN FOR INTERIOR NOISE

J. Montgomery

The Boeing Company, USA

ICAS 2008-4.9.2 INVITED

PIEZO ACTIVE VIBRATION AND NOISE CONTROL IN HELICOPTERS

P. Jaenker, V. Kloepperl*, P. Konstanzer*, et al

EADS, Germany; *Eurocopter, Germany

ICAS 2008-4.9.3

A NOVEL RECIPROCAL SOUND TRANSMISSION MEASURING METHOD, APPLIED ON A COMPOSITE FUSELAGE

H. van der Wal, P. Sijtsma, B. Berton*, et al

NLR, Netherlands; *Dassault Aviation, France

ICAS 2008-4.9.4

PROBLEMS OF VIBROACOUSTICS FOR NEW AIRPLANE GENERATION

V. Baklanov

JSC “Tupolev”, Russian Federation

ICAS 2008-5.8 Unconventional Vehicles:

Chairs: J. Ricciardi, NRC, CA

ICAS 2008-5.9 UAS Control II:

Chairs: J. Vian, The Boeing Company, US

ICAS 2008-5.8.1

PARAMETER IDENTIFICATION OF FLYING WING WITH SIGNIFICANT DEFORMATION

B. Gati, M. Somos

Budapest Univ. of Technology and Economics, Hungary

ICAS 2008-5.8.2

SIMULATION OF A NON-AXISYMMETRIC UNDERSEA VEHICLE USING A RECURSIVE NEURAL NETWORK

D. E. Hess, W. E. Faller*, J. Lee, et al

Naval Surface Warfare Center, USA; *Applied Simulation Technologies, USA

ICAS 2008-5.8.3

FLIGHT DYNAMICS OF THE FLYING WING

S. D. D'Urso, R. Martinez-Val*

Univ. Frederico II, Naples, Italy; *Universidad Politecnica de Madrid, Spain

ICAS 2008-5.9.1 INVITED

MODELING AND SIMULATION OF FLAPPING WINGS MICRO-AERIAL VEHICLES FLIGHT DYNAMICS

J. Lewitowicz, G. Kowalczyk, K. Sibilski, et al

Air Force Institute of Technology, Poland

ICAS 2008-5.9.2

ROBUST OPTIMAL DESIGN OF AN AUTOPILOT FOR TRANSITIONAL FLIGHTS OF A TAIL-SITTER MINI UAV

D. Kubo, S. Suzuki*

JAXA, Japan; *Univ. of Tokyo, Japan

ICAS 2008-5.9.3

GENETIC FUZZY CONTROL FOR AUTONOMOUS DUCTED-FAN VTOL UAV

Z. Omar, C. Bil*

UTHM Univ., Malaysia; *RMIT Univ., Australia

ICAS 2008-5.9.4

ICAS 2008-6.8 Autonomous Flight:

Chairs: N. Alley, Georgia Tech., US; G. Holmberg, Saab, SE

ICAS 2008-6.9 Aerospace and Society:

Chairs: E. Schwartz, The Boeing Company, US; L Manfriani, Zurich Univ. of Applied Sciences, CH

ICAS 2008-6.8.1 INVITED

DAMAGE TOLERANT FLIGHT CONTROL SYSTEMS FOR UNMANNED AIRCRAFT

V. Gavrilets

Rockwell Collins, USA

ICAS 2008-6.8.2 INVITED

POTENTIAL ACTIVE-VISION CONTROL SYSTEMS FOR UNMANNED AIRCRAFT

E. Johnson

Georgia Institute of Technology, USA

ICAS 2008-6.8.3 INVITED

PERSPECTIVES ON (MULTI-) UAV OPERATIONS: AUTONOMY & SECURITY ISSUES

P. Fabiani

ONERA, France

ICAS 2008-6.9.1 INVITED

EUROPE'S RESEARCH TACKLES THE GLOBAL CHALLENGES TO AERONAUTICS

D. Knoerzer

European Commission, Belgium

ICAS 2008-6.9.2

THE REGIONAL AEROSPACE CLUSTER POLICY IN EUROPE

T. Schönfeld, F. Jouaillec

Aerospace Valley, France

ICAS 2008-6.9.3

KEY EXAMPLES AND POTENTIAL OF AVIATION YOUTH PROGRAMS IN GERMANY

H. Friehmelt

Forum Luft- und Raumfahrt e.V., Germany

ICAS 2008-6.9.4

FRAMEWORK OF PAKISTAN AEROSPACE INDUSTRY QUALITY SYSTEM

M. Asim, A. Rehman

Pakistan Air Force, Pakistan

ICAS 2008-7.8 Morphing Structures:

Chairs: C. Weishäupl, EADS, DE; J. Bayandor, RMIT, AUS

ICAS 2008-7.9 Composite Design II:

Chairs: C. Guy, RMIT Univ., AUS; O. Rand, Technion, IL

ICAS 2008-7.8.1

DESIGN AND MANUFACTURING OF COMPOSITE CHIRAL STRUCTURES WITH MORPHING CAPABILITIES

P. Bettini, A. Airoldi, L. Di Landro, et al

Politecnico di Milano, Italy

ICAS 2008-7.8.2

POST-BUCKLED PRECOMPRESSED ELEMENTS: A NEW CLASS OF FLIGHT CONTROL ACTUATORS ENHANCING MORPHING WING UAVS

R. Vos

Univ. of Kansas, USA

ICAS 2008-7.8.3

APPLICATION OF SHAPE OPTIMISATION TO AIRCRAFT WING STRUCTURES

V. Anand, C. Bil

RMIT Univ., Australia

ICAS 2008-7.9.1 (AIAA 2008-8976 )

FLIGHT VEHICLE COMPOSITE STRUCTURES

E. Forster, S. Clay, R. Holzwarth, et al

AFR/WPAFB, USA

ICAS 2008-7.9.2

SURVEY OF FEASIBLE NUMERICAL APPROACHES TO ANALYSE THE BEHAVIOUR OF A COMPOSITE SKIN PANEL DURING A WATER IMPACT

E. Francesconi, M. Anghileri, L. M. L. Castelletti, et al

Politecnico di Milano, Italy

ICAS 2008-7.9.3

BWB MILITARY CARGO TRANSPORT FUSELAGE DESIGN AND ANALYSIS

S. H. Cho, C. Bil, J. Bayandor

RMIT Univ., Australia

ICAS 2008-7.9.4

THERMAL ASPECTS FOR COMPOSITE STRUCTURES - FROM MANUFACTURING TO IN-SERVICE PREDICTIONS

T. Sproewitz, J. Tessmer, T. Wille

DLR, Germany

ICAS 2008-8.8 Aviation Efficiency:

Chairs: T. Farley, NASA, US; N. Smith, NASA, US

ICAS 2008-8.9 ATM II:

Chairs: H. Offerman, LVNL, NL

ICAS 2008-8.8.1 (AIAA 2008-8951)

NETWORK ENABLED OPERATIONS ENHANCES AVIATION EFFICIENCY

M. E. Miller, R. Stamm

Raytheon Company, USA

ICAS 2008-8.8.2 (AIAA 2008-8952)

CAPACITY MODELLING FOR FUTURE AERONAUTICAL SAFETY COMMUNICATIONS OVER WIDE AREAS

H. Gonzalez-Perez, C. Bes, X. P. Menéndez*

CNES, France; *UPC, Spain

ICAS 2008-8.8.3 (AIAA 2008-8953)

PRELIMINARY ANALYSIS OF STRATEGIES AND CHALLENGES TO ENCOURAGE DATA LINK ADOPTION OVER THE NORTH ATLANTIC AIRSPACE

N. V. Campos, A. L. Weigel, R. J. Hansman

MIT, USA

ICAS 2008-8.9.1

AUTOMATED CONFLICT RESOLUTION - A SIMULATION-BASED SENSITIVITY STUDY OF AIRSPACE AND DEMAND

M. Kupfer, T. Farley*, Y. -C. Chu**, et al

Univ. of California, Santa Cruz, USA; *NASA, USA; **AerospaceComputing Inc., USA

ICAS 2008-8.9.2

ENABLING TECHNOLOGY EVALUATION FOR EFFICIENT CONTINUOUS DESCENT APPROACHES

R. J. de Muynck, L. Verhoeff, R. P. M. Verhoeven, et al

NLR, Netherlands

ICAS 2008-8.9.3

DEFINING DYNAMIC CRITICAL POINTS FOR DYNAMIC AIRSPACE CONFIGURATION

S. Zelinski

NASA, USA

ICAS 2008-8.9.4

DESIGN OF OPERATION DATABASE FOR ATM PERFORMANCE ASSESSMENT

K. Kageyama, Y. Fukuda

ENRI, Japan

ICAS 2008-9.8 Structural Damage:

Chairs: K. Hayakawa, Fujikin Inc., JP

ICAS 2008-9.9 Turbulence and Wake Vortex Detection:

Chairs: K. Sheth, NASA, US

ICAS 2008-9.8.1

SIMPLIFYING MSD MODELING BY USING CONTINUING DAMAGE ASSUMPTION AND PARAMETRIC STUDY: THE ROLE OF RIVET SQUEEZE FORCE

A. N. Garcia, A. W. S. Mello Jr., P. E. Irving*

Institute of Aeronautics and Space, Brazil; *Cranfield Univ., UK

ICAS 2008-9.8.2

STUDY ON THE RELATIONSHIP BETWEEN CORROSION DAMAGE AND RESIDUAL STRENGTH OF AL 7075-T6 ALLOY

Y. Guo, L. Wu, Q. Sun

NPU, China

ICAS 2008-9.8.3

AN ANALYTICAL MODEL FOR PREDICTION OF THE STEADY STATE CREEP DEFORMATIONS AND STRESSES OF SHORT FIBER COMPOSITES

M. Mondali, A. Abedian, G. Ghavami

Sharif Univ. of Technology, Iran

ICAS 2008-9.9.1

PILOTED SIMULATION RESULTS OF AN ONBOARD WAKE VORTEX DETECTION, WARNING AND AVOIDANCE SYSTEM AND COCKPIT DISPLAY ASPECTS

W. F. J. A. Rouwhorst, J. Groeneweg, G. Winckelmans*, et al

NLR, Netherlands; *UCL, Belgium

ICAS 2008-9.9.2

DEVELOPMENT OF AN ONBOARD DOPPLER LIDAR FOR FLIGHT SAFETY

H. Inokuchi, H. Tanaka, T. Ando*

JAXA, Japan; *Mitsubishi Electric Corporation, Japan

ICAS 2008-9.9.3

WAKE TURBULENCE MITIGATION FOR ARRIVALS (WTMA)

D. Williams, G. Lohr

NASA, USA

ICAS 2008-9.9.4

ICAS 2008-10.8 Next Generation Air Traffic System:

Chairs: R. Eveleigh, Eurocontrol, FR; S. Hasan, LMI, US

ICAS 2008-10.9 Future Air Transportation User Needs (PANEL):

Chairs: P. Kopardekar, NASA, US

ICAS 2008-10.8.1 (AIAA 2008-8924)

DEVELOPMENT AND APPLICATION OF AN INTEGRATED APPROACH TOWARD NASA AIRSPACE SYSTEMS RESEARCH

R. Barhydt, R. K. Fong, P. D. Abrahamson*, et al

NASA, USA; *PDA Associates, USA

ICAS 2008-10.8.2 (AIAA 2008-8925)

NEXTGEN AND SESAR: OPPORTUNITIES FOR UAS INTEGRATION

M. DeGarmo, D. Maroney

The MITRE Corporation, USA

ICAS 2008-10.8.3
PERFORMANCE-BASED TMA HANDLING FOR MIXED TRAFFIC USING A GROUND BASED 4D-GUIDANCE FOR UNEQUIPPED AIRCRAFT

A. Kuenz, H. Becker, C. Edinger, et al

DLR, Germany

ICAS 2008-10.9.1

ICAS 2008-10.9.2

ICAS 2008-10.9.3

ICAS 2008-10.9.4

ICAS 2008-11.8 Departure Procedures:

Chairs: B. Baxley, NASA, US

ICAS 2008-11.9 Arrival Procedures:

Chairs: D. Isaacson, NASA, US; P. Lee, San Jose State Univ./NASA Ames, US

ICAS 2008-11.8.1 (AIAA 2008-8919)

IMPROVED PREDICTION OF GATE DEPARTURE TIMES USING PRE-DEPARTURE EVENTS

L. S. Cook, S. Atkins, Y. Jung*

Mosaic ATM Inc, USA; *NASA, USA

ICAS 2008-11.8.2 (AIAA 2008-8920)

BENEFIT POTENTIAL OF CONTINUOUS CLIMB AND DESCENT OPERATIONS

P. Melby, R. H. Mayer

The MITRE Corporation, USA

ICAS 2008-11.8.3 (AIAA 2008-8921)

AIRCRAFT WAKE VORTEX SCENARIOS SIMULATION FOR TAKE-OFF AND DEPARTURE

F. Holzäpfel, J. Kladetzke, S. Amelsberg*, et al

DLR, Germany; *TU Berlin, Germany

ICAS 2008-11.9.1 (AIAA 2008-8930)

TERMINAL AREA REQUIRED TIME OF ARRIVAL (RTA) CONCEPT OF OPERATIONS AND AUTOMATION PROTOTYPE

P. V. MacWilliams, E. Zakrzewski

The MITRE Corporation, USA

ICAS 2008-11.9.2 (AIAA 2008-8931)

SIMULATION RESULTS FOR AIRBORNE PRECISION SPACING ALONG CONTINUOUS DESCENT ARRIVALS

B. E. Barmore, T. S. Abbot*, W. R. Capron**, et al

NASA, USA; *Booz Allen Hamilton, USA; **Lockheed Martin Corporation, USA

ICAS 2008-11.9.3 (AIAA 2008-8932)

ANALYSIS OF ARRIVAL MANAGEMENT PERFORMANCE WITH AIRCRAFT REQUIRED TIME OF ARRIVAL CAPABILITIES

A. Haraldsdottir, J. Scharl, J. King, et al

The Boeing Company, USA

ICAS 2008-11.9.4 (AIAA 2008-8933)

IMPACT OF ESTOL CAPABILITY ON RUNWAY CAPACITY - AN ANALYTICAL APPROACH

P. Phleps, P. Böck, C. Gologan*, et al

TU Munich, Germany; *Bauhaus Luftfahrt, Germany

 


Thursday September 18th Morning Sessions

0830 - 0930                                                                              GENERAL LECTURE IV (INVITED) - Chairman: B. Fredriksson, Sweden                                                           

Dr. N. Takeda, Tokyo Univ., Japan: RECENT DEVELOPMENT OF STRUCTURAL HEALTH MONITORING TECHNOLOGIES FOR AIRCRAFT COMPOSITE STRUCTURES (ICAS 2008-0.7)

 

0930 - 1000                                                                                                                              BREAK

1000 - 1030

1030 - 1100

1100 - 1130

1130 - 1200

1200 - 1230

 

 

 

 

 

 

 

 

 

 

 

 

 

ICAS 2008-1.10 Supersonic Aircraft Concepts: Chairs: R. Wolz, Gulfstream, US

ICAS 2008-1.10.1 INVITED

DESIGN OF A SMALL SUPERSONIC TRANSPORT AIRCRAFT WITH HIGH ENVIRONMENTAL CONSTRAINTS

P. de Saint-Martin, B Stoufflet, Y. Deremaux, et al

Dassault-Aviation, France

ICAS 2008-1.10.2

SUPERSONIC AIRCRAFT FORMATION FLYING TO INCREASE FLIGHT EFFICIENCY

R. K. Nangia, M. E. Palmer, W. Blake*, et al

Nangia Aero Research Associates, UK; *US-AFRL, USA

ICAS 2008-1.10.3

ICAS 2008-1.10.4

ICAS 2008-1.10.5

ICAS 2008-2.10 Unsteady Flow II: Chairs: D. Hummel, TU Braunschweig, DE; H. Reed, Texas A&M Univ., US

ICAS 2008-2.10.1

COMPUTATIONAL INVESTIGATION AND DESIGN OF COMPLIANT MEMBRANE WINGS FOR BIOLOGICALLY INSPIRED FLIGHT VEHICLES

D. J. Willis, E. R. Israeli, J. Peraire

MIT, USA

ICAS 2008-2.10.2

A COMPARISON OF NUMERICAL RANS SIMULATIONS AND FLOW FIELD MEASUREMENTS OF AN OSCILLATING AIRFOIL FOR FLAPPING WING PROPULSION

S. Bansmer, E. Mazlum, R. Radespiel

TU Braunschweig, Germany

ICAS 2008-2.10.3

SMALL DISTURBANCE NAVIER-STOKES COMPUTATIONS FOR LOW ASPECT RATIO WING PITCHING OSCILLATIONS

A. Pechloff, B. Laschka

TU Munich, Germany

ICAS 2008-2.10.4

PREDICTION OF HELICOPTER MANEUVER LOADS USING A TIGHTLY COUPLED CFD/CSD ANALYSIS

J. Sitaraman, B. Roget

National Institute of Aerospace, USA

ICAS 2008-2.10.5

NUMERICAL SIMULATION OF 3D FLAPPING WING BASED ON CHIMERA METHOD

W. Q. Yang, B. F. Song, W. P. Song

NPU, China

ICAS 2008-3.10 Flow Control II: Chairs: Y. Nakamura, Nagoya Univ., JP;  W. Saric, Texas A&M Univ., US

ICAS 2008-3.10.1

SUPPRESSING BOUNDARY LAYER SEPARATION BY UNSTEADY EXCITATION OF MINI-SCALE LEADING-EDGE FLAPS

X. Huang

National Research Council, Canada

ICAS 2008-3.10.2

ACTIVE CANCELLATION OF TOLLMIEN-SCHLICHTING INSTABILITIES UP TO M = 0.40

M. Engert, W. Nitsche

T U Berlin, Germany

ICAS 2008-3.10.3

TRANSVERSAL INJECTED SYNTHETIC JETS FOR WALL TURBULENCE CONTROL

M. Cannata, G. Iuso

Politecnico di Torino, Italy

ICAS 2008-3.10.4

SEPARATION CONTROL BY SYNTHETIC JET ACTUATOR IN STRAIGHT BLADE CASCADE

M. Matejka, L. Popelka*, P. Safarik, et al

Czech TU in Prague, Czech Republic; *Academy of Science of the Czech Republic, Czech Republic

ICAS 2008-3.10.5

VORTEX SHEDDING FROM A ROTATING CIRCULAR CYLINDER AT MODERATE SUB-CRITICAL REYNOLDS NUMBERS AND HIGH VELOCITY RATIO

C. Badalamenti, S. A. Prince

City Univ., UK

ICAS 2008-4.10 Environmentally Novel Concepts: Chairs: B. Shivashankara, The Boeing Company, US; F. Haselbach, Rolls-Royce, UK

ICAS 2008-4.10.1

ACHIEVING HIGHLY EFFICIENT CIVIL AVIATION - WHY & HOW WITH AIR-TO-AIR REFUELLING, REVIEW & NEW DEVELOPMENTS

R. K. Nangia

Nangia Aero Research Associates, UK

ICAS 2008-4.10.2 (AIAA 2008-8963)

COMBINATORIAL OPTIMIZATION TO INCLUDE GREENER TECHNOLOGIES IN A SHORT-TO-MEDIUM RANGE COMMERCIAL AIRCRAFT

S. Lehner, W. Crossley

Purdue Univ., USA

ICAS 2008-4.10.3

THE GREEN FREIGHTER PROJECT - OBJECTIVES AND FIRST RESULTS

K. Seeckt, W. Heinze*, D. Scholz

Hamburg Univ. of Applied Sciences, Germany; *TU Braunschweig, Germany

ICAS 2008-4.10.4

NOVEL DESIGN CONCEPTS FOR AIRCRAFT WITH REDUCED NOISE AND GLOBAL WARMING CHARACTERISTICS

S. Mistry, H. Smith, J. P. Fielding

Cranfield Univ., UK

ICAS 2008-4.10.5

A GREEN ALTERNATIVE FOR PILOT TRAINING

D. P Heatley, R. Johnston, R. Canders, et al

Queen's Univ. Belfast, UK

ICAS 2008-5.10 Safety: Chairs: Y. Tani, Kyushu Univ., JP; B. Mulder, TU Delft, NL

ICAS 2008-5.10.1

RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM – PART 1.  INTELLIGENT FLIGHT CONTROL SYSTEM

S. Suzuki, A. Yanagida*

Univ. of Tokyo, Japan; *SJAC, Japan

ICAS 2008-5.10.2

RESEARCH AND DEVELOPMENT FOR FAULT TOLERANT FLIGHT CONTROL SYSTEM - PART 2 FLIGHT EXPERIMENTS

K. Masui, H. Tomita, A. Yanagida*

JAXA, Japan; *The Society of Japanese Aerospace Companies, Japan

ICAS 2008-5.10.3

PERFORMANCE EVALUATION AND HILS TEST OF CONTROL ALLOCATION METHODS FOR RECONFIGURATION CONTROL

B. M. Min, B. J. Kim*, E. T. Kim**, et al

KAIST, Korea; *KAI, Korea; **KARI, Korea

ICAS 2008-5.10.4

NONLINEAR MODEL FOLLOWING RECONFIGURABLE FLIGHT CONTROL SYSTEM

M. T. Zugaj, J. P. Narkiewicz

Warsaw Univ. of Technology, Poland

ICAS 2008-5.10.5

THE INFLUENCE OF FREE - PLAY AND FRICTION IN CONTROL SYSTEM ON AIRCRAFT DYNAMICS

K. Sibilski, J. Zurek, W. Wroblewski*

Air Force Institute of Technology, Poland; *Wroclaw Univ. of Technology, Poland

ICAS 2008-6.10 Design Methodology II: Chairs: J. Wiggenraad, NLR, NL; W. Anemaat, Darcorp, US

ICAS 2008-6.10.1

KNOWLEDGE BASED ENGINEERING TO SUPPORT AIRCRAFT MULTIDISCIPLINARY DESIGN AND OPTIMISATION

G. La Rocca, M. J. L. van Tooren

TU Delft, Netherlands

ICAS 2008-6.10.2

SYSTEM INFRASTRUCTURE FOR INTEGRATED AND COLLABORATIVE PRODUCT DEVELOPMENT IN THE AERONAUTIC INDUSTRY

T. Nguyen Van, P. L. Frossard, P. Guellec*, et al

Snecma, France; *Airbus CIMPA, France

ICAS 2008-6.10.3

AUTOMATING THE DEVELOPMENT PROCESS OF THERMOPLASTIC COMPOSITE SHEET RIBS USING KNOWLEDGE BASED ENG. TECHNIQUES

T. van der Laan, B. Vermeulen, F. van Dalen

Stork Fokker AESP, NL

ICAS 2008-6.10.4

DEVELOPMENT AND IMPLEMENTATION OF KNOWLEDGE-BASED DESIGN PROCESS PRIMITIVES

E. J. Schut, M. J. L. van Tooren

TU Delft, Netherlands

ICAS 2008-6.10.5

METHODOLOGY OPTIMIZATION OF METAL CUTTING PROGRAMMING APPLIED TO AERONAUTICAL COMPONENTS

D. Mazzotta, A. Riccabone*

Univ. of Salento, Italy; *Politecnico di Torino, Italy

ICAS 2008-7.10 Aeroelasticity III: Chairs: D. Graham, DSTO Defence, AU; J-P. Grisval, ONERA, FR

ICAS 2008-7.10.1

ACTIVE AND PASSIVE STRUCTURAL MEASURES FOR AEROELASTIC WINGLET DESIGN

B. Nagel, M. Kintscher, T. Streit

DLR, Germany

ICAS 2008-7.10.2

DEVELOPMENT OF A RUDDERLESS AEROELASTIC FIN TECHNOLOGY

M. Trapani, S. Guo

Cranfield Univ., UK

ICAS 2008-7.10.3

OPTIMUM AEROELASTIC DESIGN OF A RESONANCE TYPE FLAPPING WING FOR MICRO AIR VEHICLES

K. Isogai, Y. Kamisawa, H. Sato

Nippon Bunri Univ., Japan

ICAS 2008-7.10.4

NUMERICAL SIMULATION OF AN OSCILLATING AND FLEXIBLE AIRFOIL FOR FLAPPING WING PROPULSION WITH FLUID-STRUCTURE INTERACTION

R. Unger, M. C. Haupt, P. Horst

TU Braunschweig, Germany

ICAS 2008-7.10.5

TRANSONIC FLUTTER ANALYSIS OF AN AIRFOIL WITH APPROXIMATE BOUNDARY METHOD

B. Zhu, Z.D. Qiao, C. Gao

NPU, China

ICAS 2008-8.10 Advances in Airbreathing Propulsion (ISABE session): Chairs: W. Whitlow, NASA, US; C. Mari, Messier-Bugatti, France;

ICAS 2008-8.10.1 INVITED

DEVELOPING THE NEXT GENERATION OF GLOBAL GAS TURBINE ENGINEERS

S. Giris

Pratt & Whitney, Canada

ICAS 2008-8.10.2 INVITED

CUTTING EDGE TECHNOLOGIES FOR DESIGN, PRODUCTION AND REPAIR OF NEXT GENERATION AERO ENGINES

R. Walther

MTU Aero Engines GmbH, Germany

ICAS 2008-8.10.3 INVITED

COUPLED HIGH-FIDELITY ENGINE SYSTEM SIMULATION

R. W. Claus, T. Lavelle, S. Townsend, et al

NASA, USA

ICAS 2008-8.10.4 INVITED

VIRTUAL ENTERPRISE COLLABORATION - BREAKTHROUGH TECHNOLOGIES PROVIDED BY VIVACE

P. Plegas, O. Isaksson, M. Lindeblad, et al

Volvo Aero, Sweden

ICAS 2008-8.10.5 INVITED

PROPULSION TECHNOLOGIES FOR THE FUTURE OF AVIATION

W. Whitlow Jr.

NASA, USA

ICAS 2008-9.10 Man Machine Interface: Chairs: D. Kulkarni, NASA, US

ICAS 2008-9.10.1

RESEARCH ON INTEGRATED COLLIMATED COCKPIT VISUAL AND FLIGHT INFORMATION SYSTEM

C. Berth, G. Hüttig, O. Lehmann

TU Berlin, Germany

ICAS 2008-9.10.2

DESIGN OF EXPERIMENT FOR THE PILOT EVALUATION OF AN AIRBORNE RUNWAY INCURSION ALERTING SYSTEM

S. Szasz, J. Gauci, D. Zammit-Mangion, et al

Cranfield Univ., UK

ICAS 2008-9.10.3

DESIGN AND EVALUATION OF A 4D INTERFACE FOR ATC

S. Bagassi, F.De Crescenzio, F. Persiani

Univ. of Bologna, Italy

ICAS 2008-9.10.4

BIOMECHANICAL PILOT PROPERTIES IDENTIFICATION BY INVERSE KINEMATICS/INVERSE DYNAMICS MULTIBODY ANALYSIS

M. Mattaboni, A. Fumagalli, M. Jump*, et al

Politecnico di Milano, Italy; *Univ. of Liverpool, UK

ICAS 2008-9.10.5

THE SIMULATION OF THE HUMAN-MACHINE PARTNERSHIP IN UCAV OPERATION

Y. C. Luan, H. J. Xue, B. F. Song

NPU, China

ICAS 2008-10.10 Future Airspace Concepts: Chairs: C. Push, Eurocontrol, FR; J. Robinson, NASA, US

ICAS 2008-10.10.1 (AIAA 2008-8935)

TOWARDS SESAR PERFORMANCE TARGETS - THE SUPER-HIGHWAY APPROACH

M. Poppe, T. Hellbach

DFS Deutsche Flugsicherung GmbH, Germany

ICAS 2008-10.10.2 (AIAA 2008-8936)

CURRENT AIRSPACE CONFIGURATION PRACTICES AND THEIR IMPLICATIONS FOR FUTURE AIRSPACE CONCEPTS

N. A. Doble, R. Hoffman, P. U. Lee*, et al

Metron Aviation Inc., USA; *SJSU / NASA,  USA

ICAS 2008-10.10.3 (AIAA 2008-8937)

IMPACT OF US-EU OPEN AREA AVIATION TREATY ON US AVIATION: A PARAMETRIC ANALYSIS WITH SIMULATION

D. Bhadra, R. Schaufele*

MITRE/CAASD, USA; *APO/FAA, USA

ICAS 2008-10.10.4 (AIAA 2008-8938)

ON-DEMAND SPECIAL USE AIRSPACE

J. Krozel, N. Gaertner, J. Prete, et al

Metron Aviation Inc., USA

ICAS 2008-10.10.5 (AIAA 2008-8939)

PRINCIPLES OF AIRSPACE TUBE DESIGN FOR DYNAMIC AIRSPACE CONFIGURATION

R. Hoffman, J. Prete

Metron Aviation Inc., USA

ICAS 2008-11.10 Traffic Flow Management II: Chairs: S. Mohleji, MITRE, US; R. Barhydt, NASA, US

ICAS 2008-11.10.1 (AIAA 2008-8940)

INTEGRATED TIME-BASED FLOW MANAGEMENT CONCEPT

S. Stalnaker, P. Ostwald, E. Beaton, et al

The MITRE Corporation, USA

ICAS 2008-11.10.2 (AIAA 2008-8941)

ANALYSIS OF GAPS BETWEEN THE PREDICTIVE AND THE ADAPTIVE COMPONENT IN ATM

C. Gwiggner, S. Nagaoka, V. Duong*

ENRI, Japan; *EUROCONTROL, France

ICAS 2008-11.10.3 (AIAA 2008-8942)

QUEUEING NETWORK MODELS OF THE NATIONAL AIRSPACE SYSTEM

M. D. Tandale, P. Sengupta, P. K. Menon, et al

Optimal Synthesis Inc., USA

ICAS 2008-11.10.4 (AIAA 2008-8943)

CONTROLLER SUPPORT FOR MANAGING HIGH-EFFICIENCY ARRIVALS IN DENSE TRAFFIC ENVIRONMENTS

T. Callantine, E. Palmer*

San Jose State Univ., USA; *NASA, USA

ICAS 2008-11.10.5 (AIAA 2008-8944)

UTILIZATION OF NETWORK THEORY FOR THE ENHANCEMENT OF ATO AIR ROUTE FORECAST

D. A. DeLaurentis, E.-P. Han, T. Kotegawa, et al

Purdue Univ., USA


Thursday September 18th Afternoon Sessions

1400 - 1430

1430 - 1500

1500 - 1530

ICAS 2008-1.11 Aviation Design: Chairs: D. Levy, Cessna, US; A. Murphy, Queen's Univ. Belfast, UK

ICAS 2008-1.11.1 (AIAA 2008-8947)

MDO DESIGN SUPPORT BY INTEGRATED ENGINEERING SERVICES WITHIN A MULTI-AGENT TASK ENVIRONMENT

J. P. T. J. Berends, M. J. L. Van Tooren

TU Delft, Netherlands

ICAS 2008-1.11.2 (AIAA 2008-8948)

A LOGICAL APPROACH FOR EVALUATING PRELIMINARY SHAPE DESIGN OF A VERY LIGHT JET

G. -H. Cho, H. -U. Park, K. -S. Jeon, et al

Konkuk Univ., Korea

ICAS 2008-1.11.3 (AIAA 2008-8950)

DEVELOPMENT OF A LANDING DRAG CHUTE SYSTEM SYSTEM FOR VERY LIGHT JETS

R. L. Thomas, D. G. Thomas*

Paratech Parachutes, USA; *Thomas Aerospace Corporation, USA

ICAS 2008-2.11 Aerodynamic Optimization II: Chairs: R. Liebeck, The Boeing Company, US

ICAS 2008-2.11.1

EFFICIENT APPROACH FOR MULTIPOINT AERODYNAMIC WING DESIGN OF BUSINESS JET AIRCRAFT

S. Peigin, B. Epstein*

Israel Aerospace Industries, Israel; *The Academic College of Tel-Aviv, Israel

ICAS 2008-2.11.2

OPTIMISING HIGH-EFFICIENCY RUDDERS FOR TRANSPORT AIRCRAFT FUEL BURN REDUCTION

M. Laban, M. H. Smaili, D. R. van der Heul, et al

NLR, Netherlands

ICAS 2008-2.11.3

AERODYNAMIC OPTIMIZATION OF AIRCRAFT CONFIGURATIONS WITH MULTIDISZIPLINARY ASPECTS

M. Hitzel, L. Nardin, K. Sorensen, et al

EADS-MAS, Germany

ICAS 2008-3.11 Flow Control III: Chairs: R. Henke, RWTH Aachen, DE

ICAS 2008-3.11.1

FLOW CONTROL TECHNIQUES FOR TRANSPORT AIRCRAFT

A. Shmilovich, Y. Yadlin

The Boeing Company, USA

ICAS 2008-3.11.2

ACTIVE SEPARATION CONTROL ON A SLATLESS 2D HIGH-LIFT  WING SECTION

F. Haucke, I. Peltzer, W. Nitsche

TU Berlin, Germany

ICAS 2008-3.11.3

AERODYNAMIC STALL SUPPRESSION ON AEROFOIL SECTIONS USING PASSIVE AIR JET VORTEX GENERATORS

S. A. Prince, V. Khodagolian, C. Singh, et al

City Univ., UK

ICAS 2008-4.11 Terminal Area Low Noise Routeing: Chairs: F. Francy, The Boeing Company, US; K. Mans, RAeS, UK

ICAS 2008-4.11.1

OPTIMIZATION OF RNAV NOISE ABATEMENT ARRIVAL TRAJECTORIES

R. H. Hogenhuis, S. J. Heblij, H. G. Visser

TU Delft, Netherlands

ICAS 2008-4.11.2

ENVIRONMENT-AWARE RUNWAY ALLOCATION ADVICE SYSTEM

J. M. Nibourg, H. H. Hesselink, Y. A. J. R. van de Vijver

NLR, Netherlands

ICAS 2008-4.11.3

TECHNOLOGY-ENABLED IMPROVEMENTS FOR TERMINAL AREA CAPACITY AND  ENVIRONMENTAL IMPACT

H. Jimenez

Georgia Institute of Technology, USA

ICAS 2008-5.11 Flight Modelling II: Chairs: K. Hui, NRC, CA

ICAS 2008-5.11.1

DYNAMIC SIMULATION OF A TOWED DECOY SYSTEM

M. C. Leijonhufvud, A. Lindberg

Saab AB, Sweden

ICAS 2008-5.11.2

MODELLING OF STATIC AERODYNAMICS OF HELICOPTER UNDERSLUNG LOADS

D. I. Greenwell

City Univ., UK

ICAS 2008-5.11.3

GROUND EFFECT MODELING FOR ROTARY-WING SIMULATION

V. Khromov, O. Rand

Technion, Israel

ICAS 2008-6.11 Life-Cycle Management: Chairs: M. Eder, Lockheed-Martin, US

ICAS 2008-6.11.1

FLEET MANAGEMENT SYSTEM FOR AN ADVANCED HELICOPTER PLATFORM - DESIGN & DEVELOPMENT REQUIREMENTS

A. Schauenburg, A. K. Sinha

RMIT Univ., Australia

ICAS 2008-6.11.2

EVALUATION OF AN INTEROPERABLE VERTICAL TAKE-OFF UAV FOR OPERATIONS WITH UGVS - AN OVERVIEW

J. Khreish, A. K. Sinha

RMIT Univ., Australia

ICAS 2008-6.11.3

KNOWLEDGE MANAGEMENT FOR THROUGH LIFE SUPPORT

L. Webb, C. Bil

RMIT Univ., Australia

ICAS 2008-7.11 Advanced Structural Analyses: Chairs: TBD

ICAS 2008-7.11.1

METHODOLOGY FOR THERMALLY INDUCED LOADING IN STRUCTURAL ANALYSIS ON THE F-35 LIGHTNING II

B. E. Mueller, R. M. Taylor

Lockheed Martin Aeronautics Company, USA

ICAS 2008-7.11.2

MECHANICS OF COMPOSITES IN LIGHTWEIGHT STRUCTURES: EFFICIENT TESTING AND COMPUTATION ACCOUNTING FOR COMPLEX 3D BEHAVIOUR

J. Tessmer, D. Hartung, L. Aschenbrenner

DLR, Germany

ICAS 2008-7.11.3

COLLAPSE BEHAVIOR OF THIN-WALLED CFRP STRUCTURES DUE TO MATERIAL AND GEOMETRIC NONLINEARITIES–EXPERIMENTS AND SIMULATION

R. Degenhardt, J. Tessmer, A. Kling

DLR, Germany

ICAS 2008-8.11 Separation and Wake Issues: Chairs: C. Golia, Seconda Università di Napoli, IT

ICAS 2008-8.11.1

AUTOMATED SEPARATION ASSURANCE IN THE PRESENCE OF UNCERTAINTY

D. McNally, D. Thipphavong

NASA, USA

ICAS 2008-8.11.2

PERFORMANCE OF THE WAKE VORTEX PREDICTION AND MONITORING SYSTEM WSVBS AT FRANKFURT AIRPORT

F. Holzäpfel, T. Gerz

DLR, Germany

ICAS 2008-8.11.3

INFORMATION REQUIREMENTS FOR SUPERVISORY AIR TRAFFIC CONTROLLERS IN SUPPORT OF A MID-TERM WAKE VORTEX DEPARTURE SYSTEM

G. Lohr, D. Williams, A. Trujillo

NASA, USA

ICAS 2008-9.11 : Traffic Flow  Management III: Chairs: TBD

ICAS 2008-9.11.1 (AIAA 2008-8946)

AN ONTOLOGY FOR TRAFFIC FLOW MANAGEMENT

B. -J. Van Putten, S. R. Wolfe*, V. Dignum

Utrecht Univ., Netherlands; *NASA, USA

ICAS 2008-9.11.2 (AIAA 2008-8945)
THE MODERNIZED NATIONAL AIRSPACE SYSTEM PERFORMANCE ANALYSIS CAPABILITY (NASPAC)

J. Post, J. Gulding, K. Noonan, et al

FAA, USA

ICAS 2008-9.11.3 (AIAA 2008-8912)
NATSIM: A SYSTEMS DYNAMICS MODEL OF NORTH ATLANTIC AIR TRAFFIC

S. Chung, K. Noonan, J. Post

FAA, USA

ICAS 2008-10.11 Innovative Concepts: Chairs: D. Rihn, Northrop Grumman, US; M. Holly, The Boeing Company, US

ICAS 2008-10.11.1 (AIAA 2008-8954 )

FLY AROUND THE WORLD WITH A SOLAR POWERED AIRPLANE

H. Ross

Solar Impulse Team, Germany

ICAS 2008-10.11.2 (AIAA 2008-8956)

MULTI-FUNCTIONAL MORPHING TRAILING EDGE FOR CONTROL OF ALL-COMPOSITE, ALL-ELECTRIC FLYING WING AIRCRAFT

A. Wildschek, M. Grünewald, R. Maier, et al

EADS, Germany

ICAS 2008-10.11.3 (AIAA 2008-8975)

A NEW APPROACH TO FORCED FLAPPING FOR THE ORNICOPTER

D. J. van Gerwen, T. van Holten

TU Delft, Netherlands

ICAS 2008-11.11 Taxi and Surface Operations: Chairs: T. Hoang, NASA, US

ICAS 2008-11.11.1 (AIAA 2008-8958)

DEPARTURE TAXI TIME PREDICTIONS USING ASDE-X SURVEILLANCE DATA

J. Legge, B. Levy

Sensis Corporation, USA

ICAS 2008-11.11.2 (AIAA 2008-8959)

SIMULATOR EVALUATION OF A NOVEL SURFACE MOVEMENT AWARENESS AND ALERTING SYSTEM (SMAAS) FOR RUNWAY INCURSION AVOIDANCE

C. Vernaleken, C. Urvoy, U. Klingauf

TU Darmstadt, Germany

ICAS 2008-11.11.3 (AIAA 2008-8960)

IMPLICATION OF VARIABILITY IN AIRPORT SURFACE OPERATIONS ON 4-D TRAJECTORY PLANNING

S. Atkins, C. Brinton, Y. Jung*

Mosaic ATM Inc., USA; *NASA, USA

1530 - 1600                                                                                                                   BREAK

1600 - 1700                                               VON KARMAN LECTURE (INVITED) - Chairman: I. Poll, Chairman ICAS Programme Committee, United Kingdom

Mr. M. Jenks, VP Boeing Commercial Airplanes, The Boeing Company, USA: THE BOEING 787 DREAMLINER PROGRAMME (ICAS 2008-0.8 

 

 

1700 - 1730                                                                                                         CLOSING CEREMONY