ACCEPTED PAPERS - CATEGORY C – POSTERS These papers will be presented in the Poster area Most papers will also appear in the congress CD proceedings
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1. AIRCRAFT AND SYSTEMS INTEGRATION
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ICAS2010-P1.1: L. -M. Fan, X. -M. Fan, Z. -B. Jiang, et al, BATRC, China; *School of Baobu Car Manage, China |
ICAS2010-P1.2: K. W. Reynolds, I. M. Kroo, Stanford Univ., USA MULTI-OBJECTIVE OPTIMIZATION OF MANNED AND UNMANNED ELECTRIC AIRCRAFT FOR MAXIMUM RANGE AND SPEED |
ICAS2010-P1.3: T. Mulyanto, H. P. Thien, H. Muhammad, Institute of Technology Bandung, Indonesia CONFIGURATION STUDY OF A COAXIAL ROTOR MAV BASED ON DYNAMIC MODEL |
2. AERODYNAMICS
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ICAS2010-P2.1: A. P. Kuryachii, D. A. Rusyanov, TsAGI, Russian Federation TURBULENT SKIN FRICTION REDUCTION OWING TO ELECTROHYDRODYNAMIC INTERACTION IN UNIPOLAR CHARGED FLUID |
ICAS2010-P2.2: H. B. Hao, Y. Yang, NPU, China |
ICAS2010-P2.3: S. -H. Zuo, Y. Yang, D. Li, NPU, China EXPERIMENTS OF CROSS-FLOW INSTABILITY IN A SWEPT-WING BOUNDARY LAYER |
ICAS2010-P2.4: Y. H. Guo, Y. Yang, Z. J. Duan, NPU, China |
ICAS2010-P2.5: Z. M. Tian, Q. Lin, G. Yang*, Tsinghua Univ., China; *AIRDC, China |
ICAS2010-P2.6: J. Z. Chai, X. Gao, Q. Li, AVIC, China HIGH-TEMPERATURE IONIZED AIR RADIATION SIMULATION ON UNSTRUCTURED GRIDS |
ICAS2010-P2.7: S. Munawar, National Univ. of Sciences and Technology, Pakistan ANALYSIS OF GRID FINS AS EFFICIENT CONTROL SURFACE IN COMPARISON TO CONVENTIONAL PLANAR FINS |
ICAS2010-P2.8: G.N Li, F.W Li, Z.H Zhou, NPU, China A MULTI-BLOCK FLOW SOLVER CODE ACCELERATING WITH MULTI-GRID TECHNIQUE |
ICAS2010-P2.9: L. F. Bergamo, E. M. Gennaro, M. A. F. de Medeiros, Univ. of São Paulo, Brazil COMPUTATIONAL SIMULATION OF NOISE GENERATED AERODYNAMICALLY VIA DNS AND ACOUSTIC ANALOGY |
ICAS2010-P2.10: A Obraz, Moscow Institute of Physics and Technology, Russian Federation PREDICTION OF LAMINAR-TURBULENT TRANSITION REYNOLDS NUMBERS FOR COMPRESSIBLE BOUNDARY LAYERS |
ICAS2010-P2.11: X. Zhang, C. Zhou, Harbin Institute of Technology, China |
ICAS2010-P2.12: V. Malatesta, M. Augusto Faraco de Medeiros, Univ. of São Paulo, Brazil NUMERICAL SIMULATION OF THE MIXING LAYER GENERATED BY THE SLAT |
ICAS2010-P2.13: N. Mirkov, B. Rasuo*, Institute of Nuclear Sciences "Vinca", Serbia; *Univ. of Belgrade, Serbia NUMERICAL SIMULATION OF AIR JET ATTACHMENT TO CONVEX WALLS AND APPLICATIONS |
ICAS2010-P2.14: A. G. Rumyantsev, V. A. Silantyev, Siberian Aeronautical Research Institute, Russian Federation DESIGN OPTIMIZATION OF HIGH LIFT CONFIGURATIONS BASED ON NAVIER-STOKES EQUATIONS |
ICAS2010-P2.15: R. Cosin, F. M. Catalano, L. G. N. Correa, et al, Univ. of São Paulo, Brazil AERODYNAMIC ANALYSIS OF MULTI-WINGLETS FOR LOW SPEED AIRCRAFTS |
ICAS2010-P2.16: G. H. Kim, Y. D. Jeong, S. O. Park, KAIST, Korea MEASUREMENT AND PREDICTION OF CONTROL VANE FORCE IN THE WAKE OF A SHROUDED PROPELLER SYSTEM |
ICAS2010-P2.17: T. Ishide, N. Nishikawa*, Kisarazu National College of Technology, Japan; *Chiba Univ., Japan |
ICAS2010-P2.18: E. B. Vasilevskiy, L. V. Yakovleva, TsAGI, Russian Federation |
ICAS2010-P2.19: L. G. N. Correa, R. M. U. Entz, R. Cosin, et al, Univ. of São Paulo, Brazil |
ICAS2010-P2.20: J. Stults, R. Huffman, US Air Force Institute of Technology, USA MICROWAVE TOMOGRAPHY OF AN ATMOSPHERIC PRESSURE DIELECTRIC BARRIER DISCHARGE |
ICAS2010-P2.21: E. Hallberg, United States Naval Academy, USA ANALYSIS OF TARGETING POD EFFECTS ON ADJACENT STORES |
ICAS2010-P2.22: R. Bura, Institut Teknologi Bandung, Indonesia TURBULENCE MODEL COMPARISONS FOR SHOCK CONTROL BUMP ON A TRANSONIC AIRFOIL |
ICAS2010-P2.23: U. Jung, C. Breitsamter, TU Munich, Germany AERODYNAMIC WAKE INVESTIGATIONS OF HIGH-LIFT TRANSPORT AIRCRAFT WITH DEPLOYED SPOILERS |
ICAS2010-P2.24: H. Otsu, Y. Kamada*, Y. Yamagiwa*, et al, Ryukoku Univ., Japan; *Shizuoka Univ., Japan; **Hirobo ltd., Japan; ***JAXA, Japan |
ICAS2010-P2.25: H. D. Cerón-Muñoz, F. M. Catalano, Univ. of São Paulo, Brazil AERODYNAMIC INTERFERENCE OF A POWER-PLANT SYSTEM ON A BLENDED WING BODY CONFIGURATION |
ICAS2010-P2.26: M. Neamtu, S. Nebancea, INCAS, Romania FAST METHOD FOR AERODYNAMIC INTERFERENCE CALCULATION OF MULTIPLE SURFACE-BODY COMBINATIONS IN SUBSONIC FLOW |
3. MATERIALS AND STRUCTURES
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ICAS2010-P3.1: A. -N. Tang, Z. -T. Zhou, J. -T. Cao, Chinese Flight Test Establishment, China A TECHNIQUE OF LANDING GEAR LOADS CALIBRATION WITH STRAIN GAUGES |
ICAS2010-P3.2: X. H. Wang, Y. Yao, S. P. Cheng, Beijing Univ., China |
ICAS2010-P3.3: M. F. A. Rahman, R. D. Mohammed, X. Yu*, et al, RMIT Univ., Australia; *DSTO, Australia |
ICAS2010-P3.4: U. H. Tiong, G. Clark, RMIT Univ. & DMTC, Australia CRITICAL STRAIN PERFORMANCE OF COATING SYSTEMS AT AIRCRAFT JOINTS |
ICAS2010-P3.5 Y. Badrukhin, Siberian Aeronautical Research Institute, Russian Federation NONLINEAR ANALYSIS BY STRENGTH EVALUATION AND FABRICATION METHOD OF THIN-WALLED AIRFRAMES |
ICAS2010-P3.6: A. C. Orifici, I. Herszberg*, RMIT Univ., Australia; *CRC-ACS Ltd, Australia AN EXPERIMENTAL INVESTIGATION INTO DAMAGE MODES AND SCALE EFFECTS IN CFRP OPEN HOLE TENSION COUPONS |
ICAS2010-P3.7: Z. Wang, Y. Y. Wang, Beijing Aeronautical Technology Research Center, China A STUDY OF THE METHOD FOR CALCULATING FATIGUE DAMAGE OF AIRCRAFT BY USING RECORDED LOAD FACTORS |
ICAS2010-P3.8: M. Badiey, A. Abedian, Sharif Univ. of Technology, Iran |
ICAS2010-P3.9: F. H. Dezfuli, S. Khalilian, A. Abedian, Sharif Univ. of Technology, Iran DYNAMIC CONTROL OF PLATE WITH EMBEDDED SHAPE MEMORY ALLOY WIRES |
ICAS2010-P3.10: A. Tronche, Albert & Duval, France NEW GRADES IN STAINLESS STEELS, ALUMINIUM & TITANIUM ALLOYS FOR AERO-STRUCTURES |
4. PROPULSION
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ICAS2010-P4.1: Y. R. Ma, Chinese Flight Test Establishment, China FLIGHT TEST TO VALIDATE ENGINE SURGE-ELIMINATING SYSTEM USING DISTURBED BOARD ON FLIGHT TEST BED |
ICAS2010-P4.2: M. Chen, Beihang Univ., China CONTROL LAW DESIGN OF A MA 3.5, MIXED FLOW, AFTERBURNING,TWO-SPOOL TURBOFAN ENGINE |
ICAS2010-P4.3: L. Cho, S. Lee, J. Cho, Hanyang Univ., Korea NUMERICAL AND EXPERIMENTAL ANALYSES OF THE DUCTED FAN FOR THE SMALL VTOL UAV PROPULSION |
ICAS2010-P4.4: L. Pintat, R. Royan, R. Martet, et al, Snecma, France LOW PRESSURE TURBINE DESIGN TIME AND PERFORMANCE IMPROVEMENT USING MULTIDISCIPLINARY OPTIMIZATION AND DETAILED CAD MODEL |
ICAS2010-P4.5: C. Fureby, E. Fedina, FOI, Sweden A COMPUTATIONAL STUDY OF A MULTI-BURNER ANNULAR AERO GAS TURBINE |
5. FLIGHT DYNAMICS AND CONTROL
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ICAS2010-P5.1: M. Sato, T. Hagiwara, JAXA, Japan IN-FLIGHT SIMULATOR CONTROLLER DESIGN AND EXPERIMENTAL RESULT |
ICAS2010-P5.2: R. K. Nangia, M. E. Palmer, Nangia Aero Research, UK |
6. SYSTEMS, SUBSYSTEMS AND EQUIPMENT
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ICAS2010-P6.1: Y. Zhu, Beijing Aeronautical Technology Research Center, China MODELING OF RADAR DETECTION RANGE WITH JAMMING |
ICAS2010-P6.2: M. Jie, Y. Zhu, Q. Gao, Beijing Aeronautical Technology Research Center, China AN EFFECTS EVALUATION METHOD ON AM ANGLE DECEPTION JAMMING |
ICAS2010-P6.3: C. L. Wang, J. G. Wang, S. M. Hong, Beijing Aeronautical Technology Research Center, China ANTI-JAMMING CAPABILITY EVALUATION OF COHERENT SIDELOBE CANCELLATION |
ICAS2010-P6.4: H. Jin, J. -Y. Ki, S. -H. Kho, et al, Easy Gas Turbine Co., Ltd., Korea FLOW CHARACTERISTICS OF CIRCUMFERENTIALLY ARRAYED CIRCULAR MULTIPLE |
ICAS2010-P6.5: Y. -J. Yoo, S. -H. Kho*, J. -Y. Ki*, et al, Agency for Defense Development, Korea; *Easy Gas Turbine Co., Korea; **Firstec Co., Korea A STUDY ON THE CONCEPTUAL DESIGN OF ENVIRONMENTAL CONTROL SYSTEM WITH MODELING AND SIMULATION S/W |
ICAS2010-P6.6: H. Kobayashi, A. Nishizawa, JAXA, Japan DECREASE IN GROUND-RUN DISTANCE OF AIRPLANES BY APPLYING ELECTRICALLY-DRIVEN WHEELS |
ICAS2010-P6.7: D. Jwo, Y. Chang, F. Chung, National Taiwan Ocean Univ., Taiwan, China GPS RECEIVER CODE TRACKING LOOP DESIGNS USING THE NONLINEAR FILTERS |
ICAS2010-P6.8: H. Zhang, F. Mollet, S. Breban, et al, L2EP, France; *Hispano-Suiza, France |
ICAS2010-P6.9: Y. Jianyuan, L. Hanghang, G. Liangmin, Beijing Aeronautical Technology Research Center, China STUDY AND APPLICATION OF THE AIRBORNE VERTICAL ATMOSPHERIC PROFILING SYSTEM'S INSTALLATION ON AIRCRAFT |
ICAS2010-P6.10: R. Meuret, O. Berry*, F. Dubois, et al, Hispano-Suiza, France; *Nancy Univ., France; **Univ. de Lyon, France; ***Univ.de Lyon, France |
ICAS2010-P6.11: L. Borello, P. Maggiore, G. Villero, et al, Politecnico di Torino, Italy A COMPARISON BETWEEN DRY FRICTION DISCONTINUOUS COMPUTATIONAL ALGORITHMS |
ICAS2010-P6.12: J. Larsson, R. Ekrot, Saab AB, Sweden |
ICAS2010-P6.13: P. Rosati, S. Ricci*, A. Scotti*, et al, Centro Soccorso Alpino di Trento, Italy; *Politecnico di Milano, Italy; **Kong s.p.a., Italy ACTIVE STRETCHER CONTROL DEVICE FOR IMPROVING MOUNTAIN S.A.R. HELICOPTER MISSIONS |
ICAS2010-P6.14: Y. I. Jenie, H. Mohamad, B. Sabastian, et al, Institute of Technology Bandung, Indonesia |
7. SYSTEMS ENGINEERING AND SUPPLY CHAIN
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ICAS2010-P7.1: C. Van der Velden, H. -L. Zhang, X. Yu, et al, RMIT Univ., Australia; *GKN Aerospace Engineering Services Pty Ltd, Australia |
ICAS2010-P7.2: T. Kosmider, K. Santarek, TECHNOLOGY PARTNERS Foundation, Poland STRUCTURAL OPTION FOR FOSTERING INNOVATION IN THE AEROSPACE AND AVIATION INDUSTRIES |
ICAS2010-P7.3: A. Pozzetti, C. Bil, G. Clark, RMIT Univ., Australia IMPLEMENTATION OF PERFORMANCE BASED SYSTEM ASSESSMENT OF MILITARY MULTI-MISSION PLATFORMS |
8. AIR TRANSPORT SYSTEM EFFICIENCY
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ICAS2010-P8.1: M. Zanin, Innaxis Foundation & Research Institute, Spain |
ICAS2010-P8.2: H. F. Wang, B. Huang*, J. W. Liu, et al, Beijing Aviation Meteorological Inst., China; *Beijing Aviation Meteorological Inst. & Physical Inst. Peiking Univ., China THE EXPERIMENTAL FORECAST FOR AIRPORT TOTAL CLOUD COVER USING THE LINEAR AND NONLINEAR MODULES |
ICAS2010-P8.3: M. Groppe, R. Pagliari, D. Harris, Cranfield Univ., Germany |
ICAS2010-P8.4: K. O. Ploetner, TU Munich, Germany SIMULATION OF PASSENGER DEMAND FOR FUTURE AIR TRANSPORT CONCEPTS WITH CHANGED BLOCK TIMES |
ICAS2010-P8.5: M. Schultz, n/a Fricke, TU Dresden, Germany EVALUATION OF IMPROVED AIRPORT EMERGENCY PROCEDURES CONSIDERING PASSENGER BEHAVIOR |
9. SAFETY AND SECURITY
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ICAS2010-P9.1: L. Brown, Western Michigan Univ., USA |
ICAS2010-P9.2: Y. T. He, W. J. Shu, R. H. Cui, et al, Air Force Engineering Univ., China AN ASSESSMENT MODEL OF AIRCRAFT STRUCTURAL SAFETY BASED ON ROUGH SET THEORY |
ICAS2010-P9.3: C. M. Geacar, Politehnica Univ. Bucharest, Romania REDUCING PILOT / ATC COMMUNICATION ERRORS USING VOICE RECOGNITION |
ICAS2010-P9.4: L. Brown, Western Michigan Univ., USA IN-FLIGHT SECURITY ONBOARD COMMERCIAL AIRCRAFT: CRITICAL IMPROVEMENTS NEEDED |
ICAS2010-P9.5: M. Asim, N. Ehsan, K. Rafique, CASE, Pakistan PROBABLE CAUSAL FACTORS IN UAV ACCIDENTS BASED ON HUMAN FACTOR ANALYSIS AND CLASSIFICATION SYSTEM |