Laminar boundary layer stability experiments on a cone at Mach 8. III - Sharp cone at angle of attack
Author:
Affiliation:
1. USAF, Wright Aeronautical Laboratories, Wright-Patterson AFB, OH
2. Arnold Engineering Development Center,Arnold AF Station, TN
3. ARVIN/CALSPAN Field Services, Inc., Arnold AF Station, TN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-492
Reference36 articles.
1. Stetson, K. F., Thompson, E. R., Donaldcnn. J. C. and Siler. L. G. "Laminar . Boundary iayer Stability Experiments on a Cone at Mach 8, Part 1: Paper No. 83-1761, July 1983.
2. Shock tunnel investigation of boundary-layer transition at M equals 5.5.
3. Mach 6 Experiments of Transition on a Cone at Angle of Attack
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