Roll Moment Characteristics of Supersonic Flight Vehicle Equipped with Asymmetric Protuberance
Author:
Affiliation:
1. Department of System Integration, Yokohama National University
2. Institute of Space and Astronautical Science, JAXA
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tastj/17/2/17_17.111/_pdf
Reference16 articles.
1. 2) Kitamura, K., Fujimoto, K., Nonaka, S., Irikado, T., Fukuzoe, M., and Shima, E.: Wind Tunnel Tests on Aerodynamic Characteristics of Advanced Solid Rocket, Trans. JSASS. Aerospace Technology. Japan, 9 (2010), pp.9-14 (in Japanese).
2. 3) Kitamura, K., Fujimoto, K., Kuzuo, K., Nonaka, S., Irikado, T., Fukuzoe, M., and Shima, E.: Numerical Analysis on Aerodynamic Characteristics of Advanced Solid Rocket, Trans. JSASS. Aerospace Technology. Japan, 10 (2011), pp.1-10 (in Japanese).
3. 4) Panda, J., Martin, F. W., and Sutliff, D. L.: Estimation of the Unsteady Aerodynamics Load on Space Shuttle External Tank Protuberances from a Component Wind Tunnel Test, AIAA Paper 2008-0232, 2008.
4. 5) Iizuka, N., Fujii, K., Fujimatsu, N., and Moriya, K.: CFD Analysis of the Rolling Moment Characteristics of M-V-5 Rocket, ISTS 2004-e-11, 24th International Symposium on Space Technology and Science, Miyazaki, Japan, Jun. 2004.
5. 6) Aso, S., Maekawa, S., Karashima, K., and Sato, K.: The Experimental Studies on the Shock Wave/Turbulent Boundary Layer Interaction Region Induced by the Blunt Protuberance, JSASS J., 44 (1996), pp. 735-740 (in Japanese).
Cited by 2 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. Side Force Characteristics of Slender-Bodied Supersonic Vehicle with Two Protuberances;Journal of Spacecraft and Rockets;2022-09
2. Experimental and Numerical Investigations of Slender Body Side Force with Asymmetric Protuberances;Journal of Spacecraft and Rockets;2019-09
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