Analytical solutions for hypersonic flow past slender power-law bodies at small angle of attack

Author:

Merlen A.1,Andriamanalina D.1

Affiliation:

1. Office National d'Etudes et de Recherches Aerospatiales, 59000 Lille, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 7 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. Parametric Study on Lateral–Directional Stability of Hypersonic Waverider;AIAA Journal;2021-06-14

2. Design of Modular, Shape-transitioning Inlets for a Conical Hypersonic Vehicle;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

3. Power-Law Shaped Leading Edges in Rarefied Hypersonic Flow;Journal of Spacecraft and Rockets;2002-11

4. Power law shaped leading edges in rarefied hypersonic flow;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14

5. Differential interferometry for studying hypersonic flows;Experiments in Fluids;1996-02

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