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Numerical Study of the Receptivity of a Blunt Cone to Hypersonic Freestream Pulse Disturbances
作者: Simon He ,
Xiaolin Zhong
DOI:
10.2514/6.2021-0742
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参考文章
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Ponnampalam Balakumar, Michael Kegerise,
Receptivity of Hypersonic Boundary Layers to Acoustic and Vortical Disturbances
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
,(2011) ,
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4.
XIAOLIN ZHONG, YANBAO MA,
Boundary-layer receptivity of Mach 7.99 flow over a blunt cone to free-stream acoustic waves
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,vol. 556, pp. 55- 103 ,(2006) ,
10.1017/S0022112006009293
5.
Mujeeb Malik, Ponnampalam Balakumar,
Receptivity of Supersonic Boundary Layers to Acoustic Disturbances
35th AIAA Fluid Dynamics Conference and Exhibit.
,(2005) ,
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6.
Jia Lei, Xiaolin Zhong,
Linear Stability Analysis of Nose Bluntness Effects on Hypersonic Boundary Layer Transition
Journal of Spacecraft and Rockets.
,vol. 49, pp. 24- 37 ,(2012) ,
10.2514/1.52616
7.
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Low-storage Runge-Kutta schemes
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,vol. 35, pp. 48- 56 ,(1980) ,
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8.
Alexander Fedorov, Anatoli Tumin,
High-Speed Boundary-Layer Instability: Old Terminology and a New Framework
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,vol. 49, pp. 1647- 1657 ,(2011) ,
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9.
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Interaction of Linear Waves with Oblique Shock Waves
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,vol. 11, pp. 2350- 2362 ,(1968) ,
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Variable N-Factor Method for Transition Prediction in Three-Dimensional Boundary Layers
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,vol. 38, pp. 211- 216 ,(2000) ,
10.2514/2.973
来源期刊
AIAA Scitech 2021 Forum
American Institute of Aeronautics and Astronautics
2021 年,
Volume: , Issue: ,
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