Low Speed Stability Analysis of a Hypersonic Vehicle Design Using CFD and Wind Tunnel Testing-Reference-Cited by-同舟云学术

Low Speed Stability Analysis of a Hypersonic Vehicle Design Using CFD and Wind Tunnel Testing

Published:2017-03-02 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA International Space Planes and Hypersonics Technologies Conference
language:
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Author:

Jeyaratnam Jonathan¹,Bykerk Tamas¹,Verstraete Dries¹

Affiliation:

1. University of Sydney

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2223

Reference15 articles.

1. Active Control of Aerothermoelastic Effects for a Conceptual Hypersonic Aircraft

2. Aerodynamic and aerothermodynamic trade-off analysis of a small hypersonic flying test bed

3. Multidisciplinary Optimization of Airbreathing Hypersonic Vehicles

4. Hypersonic aircraft and their aerodynamic problems

5. Bowman, J. and Grantham, W. “Low-Speed Aerodynamic Charactersitics of a Model of a Hypersonic Research Airplane at AnglesofAttackupto90foraRangeofReynoldsNumbers,”Tech.Rep.TechnicalNoteD-403,NASA,1960.

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