| Names |
Title |
ICAS Paper Number |
| Neiland V. Y., Belov I. F. , Grechko I. Y., Yennak Y. N |
ANALYTICAL AND EXPERIMENTAL INVESTIGATIONS OF AN IMPROVED AERODYNAMIC ORBITER CONFIGURATION |
ICAS-98-R.1.2 |
| Campos L. M. B. C. |
AN ANALYTICAL APPROACH TO HIGH-ORDER, NON LINEAR AIRPLANE STABILITY PROBLEMS |
ICAS-98-R.1.7.1 |
| Smalko Z., Jazwinski J., Zurek J. |
APPLICATION OF EXPERT METHODS TO RISK ASSESSMENT OF AIR TRANSPORT SYSTEMS |
ICAS-98-R.1.9.2 |
| Oliva A. P. |
HELICOPTER REDUNDANT STATION KEEPING FLIGHT CONTROL LAW |
ICAS-98-R.1.10 |
| Riabov V. V., Yegorov I. V., Yegorova M. V. |
AEROTHERMODYNAMIC CHARACTERISTICS OF TWO-DIMENSIONAL BLUFF BODIES IN HYPERSONIC VISCOUS FLOWS |
ICAS-98-R.2.1 |
| Talbot-Stern J. L., Auld D. J. |
DIRECT SIMULATION (MONTE CARLO) OF DELTA WINGS IN THREE-DIMENSIONAL, NEAR-CONTINUUM, SUBSONIC FLOWS |
ICAS-98-R.2.2 |
| Byzov V. N. |
FLIGHT RESEARCHES OF VISCOSITY INFLUENCE ON SHARP CONES AERODYNAMICAL CHARACTERISTICS IN HYPERSONIC LOW DENSITY FLOW |
ICAS-98-R.3.3 |
| Rasuo B. |
AN EXPERIMENTAL AND THEORETICAL STUDY OF TRANSONIC FLOW ABOUT THE NACA 0012 AIRFOIL |
ICAS-98-R.3.8 |
| Vieira R., Azevedo J. L. F., Fico G. C. R., Basso E. |
THREE DIMENSIONAL FLOW SIMULATION IN THE TEST SECTION OF A SLOTTED TRANSONIC WIND TUNNEL |
ICAS-98-R.3.11 |
| Ryzhova T. B. |
ULTRASONIC ASSESSMENT OF THE RADIAL CLEARANCE OF RIVETED JOINTS IN AIRCRAFT STRUCTURES |
ICAS-98-R.4.2 |
| van Beek J. A. B. |
DYNAMIC SEAT TESTING AND HEAD INJURY CRITERIA-AN AIRCRAFT MANUFACTURER'S EXPERIENCE AND A VIEW ON THE FUTURE |
ICAS-98-R.4.5 |
| Jacob K. A., Prabhakaran V., Saravanan P. M. |
PROBABILISTIC APPROACH FOR DESIGN OF A COMPOSITE RPV WING |
ICAS-98-R.4.7 |
| Yuceoglu U., Ozerciyes V. |
FREE FLEXURAL VIBRATIONS OF COMPOSITE PLATES OR PANELS STIFFENED BY A CENTRAL OR NON-CENTRAL PLATE STRIP - SOME COMPARISONS |
ICAS-98-R.4.11 |
| Ruotolo R., Surace C. |
ON-LINE HEALTH MONITORING OF AERONAUTICAL STRUCTURES USING A VIBRATION BASED METHOD |
ICAS-98-R.5.1 |
| Sanderson S., Rose L. F. R., Callinan R. J. |
ANALYSIS OF THE INTERACTION EFFECT FOR BONDED REPAIRS |
ICAS-98-R.5.3 |
| Song B. F., Ren H., Li W. J., Lu Z. Z. |
THE METHOD FOR COMPUTING THE FAILURE PROBABILITY OF AIRCRAFT STRUCTURES |
ICAS-98-R.5.7 |
| Ahmed S. A., Abidogun K. |
THE FLOWFIELD CHARACTERISTICS OF A CONFINED SWIRLING FLOW |
ICAS-98-R.5.9 |
| Li X., Shen G., Liu J. |
A NEW, AVAILABLE HIGH-PRECISION CCD ANGLE-MEASURING SENSOR IN AERONAUTICS AND ASTRONAUTICS |
ICAS-98-R.5.11 |
| Walter S., Feirertag F. |
CAST AIRFRAME PRIMARY STRUCTURE |
ICAS-98-R.6.1 |
| Leacock, G. R., Thomson D. G. |
ESTIMATION OF PILOT MODEL PARAMETERS FOR HELICOPTER HANDLING QUALITIES STUDIES |
ICAS-98-R.6.3 |
| Fedunov B. E. |
ON-BOARD OPERATIVE ADVICED EXPERT SYSTEMS FOR ONE-SEAT AIRCRAFTS AND STRUCTURE OF THEIR KNOWLEDGE BASES |
ICAS-98-R.6.8 |