Supersonic noncircular missile computations
Author:
Affiliation:
1. U.S. Naval Surface Warfare Center, Silver Spring, Maryland
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26047
Reference4 articles.
1. Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas Effects
Cited by 5 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. Shape Optimization of the Cross-Section for Noncircular Hypersonic Missile Forebody;International Journal of Aerospace Engineering;2020-10-23
2. Fin dihedral effects on wing-body carryover for supersonic noncircular missiles;Journal of Spacecraft and Rockets;1995-05
3. Wing-body carryover for noncircular missiles;Journal of Spacecraft and Rockets;1995-05
4. Multiple‐Zone Potential Solution around Wing‐Body Configurations;Journal of Aerospace Engineering;1993-10
5. Induced roll computations for conventional missiles;Journal of Spacecraft and Rockets;1990-09
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