Physical and Numerical Aspects of Simulating Rarefied Hypersonic Wedge Flow
Author:
Affiliation:
1. National Institute for Space Research, 12630-000 Cachoeira Paulista, Brazil
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.47875
Reference26 articles.
1. Aerodynamic Problems of Manned Space Vehicles
2. Flat-Faced Leading-Edge Effects in Low-Density Hypersonic Wedge Flow
3. Effects of compressibility on aerodynamic surface quantities over low-density hypersonic wedge flow
4. Bluntness Impact on Lift-to-Drag Ratio of Hypersonic Wedge Flow
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. Non-Rankine–Hugoniot Shock Zone of Mach Reflection in Hypersonic Rarefied Flows;Journal of Spacecraft and Rockets;2016-07
2. Bluntness Effects on Lift-to-Drag Ratio of Leading Edges for Hypersonic Waverider Configurations;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24
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