Experimental Study of Second-Mode Instabilities on a 7-Degree Cone at Mach 6-Reference-Cited by-同舟云学术

Experimental Study of Second-Mode Instabilities on a 7-Degree Cone at Mach 6

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:41st AIAA Fluid Dynamics Conference and Exhibit
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Author:

Rufer Shann¹,Berridge Dennis²

Affiliation:

1. NASA Langley Research Center

2. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3877

Reference30 articles.

1. 1Mack,L.M."Boundary-LayerLinearStabilityTheory,"SpecialCourseonStabilityandTransitionof Laminar Flow,AGARD-R-709,chap.3,June1984,pp.3-1:3-81.

2. 2Stetson,K.,Kimmel,R.,Thompson,E.,Donaldson,J.,andSiler,L."AComparisonofPlanarandConical BoundaryLayerStabilityata MachNumberof8,"AIAAPaper91-1639,June1991.

3. Example of Second-Mode Instability Dominance at a Mach Number of 5.2

4. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies

5. 5Rufer,S.J.,andSchneider,S.P."Hot-WireMeasurementsofInstabilityWavesonConesatMach6,"AIAA Paper2006-3054,June2006.

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