Secondary Instability of Stationary Crossflow Vortices on an Inclined Cone at Mach 6-Reference-Cited by-同舟云学术

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Secondary Instability of Stationary Crossflow Vortices on an Inclined Cone at Mach 6

Published:2015-06-18 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Fluid Dynamics Conference
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Author:

Ward Christopher¹,Henderson Ryan¹,Schneider Steven P.¹

Affiliation:

1. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2773

Reference21 articles.

1. 1Tirtey, S. C., Characterization of a Transitional Hypersonic Boundary Layer in Wind Tunnel and Flight Conditions, Ph.D. thesis,Von Karman Institute for Fluid Dynamics, Brussels, Belgium, August 2006.

2. Linear Stability Theory Applied to Boundary Layers

3. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS

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4. Experimental study of the high-frequency instability in the hypersonic boundary layer over a cone at 6° angle of attack;Acta Mechanica Sinica;2022-07-12

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