Author:
TSUTSUMI Seiji,TAKAKI Ryoji,TAKAMA Yoshiki,IMAGAWA Kentaro,NAKAKITA Kazuyuki,KATO Hiroyuki
Publisher
Japan Society for Aeronautical and Space Sciences
Reference22 articles.
1. 2) Cockburn, J. A. and Robertson, J. E.: Vibration Response of Spacecraft Shrouds to In-Flight Fluctuating Pressures, J. Sound Vib., 33 (1974), pp. 399-425.
2. 3) Imperatore, B., Guj, G., Ragni, A., Pizzicaroli, A. and Giulietti, E.: Aeroacoustic of the VEGA Launcher Wind Tunnel Tests and Full Scale Extrapolations, AIAA Paper 2005-2931, 2005.
3. 4) Panda, J., Martin, F. W. and Sutliff, D. L.: Estimation of the Unsteady Aerodynamic Load on Space Shuttle External Tank Protuberances from a Component Wind Tunnel Test, AIAA Paper 2008-232, 2008.
4. 5) Walker, B. E., Panda, J. and Sutliff, D. L.: Vibration Analysis of the Space Shuttle External Tank Cable Tray Flight Data with and without PAL Ramp, AIAA Paper 2008-312, 2008.
Cited by
1 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. マッハ0.7および1.3における細長物体横力特性への突起サイズの影響;AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2023