A comparison of planar and conical boundary layer stability and transition at a Mach number of 8
Author:
Affiliation:
1. USAF, Wright Laboratory, Wright-Patterson AFB, OH
2. Calspan Corp., Arnold AFB, TN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1639
Reference29 articles.
1. Measurements and Correlations of Transition Reynolds Numbers on Sharp Slender Cones at High Speeds
2. Linear Stability Theory and the Problem of Supersonic Boundary- Layer Transition
3. Mack,L.M."Boundary-LayerStabilityAnalysisfor SharpConesat Zero Angle of Attack,"AFWALTR-87-3022, August 1986.
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