Boundary-layer transition experiments on sharp, slender cones in supersonic freeflight
Author:
Affiliation:
1. U.S. Naval Surface Weapons Center, Silver Spring, Md.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1978-1129
Reference47 articles.
1. Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.
2. Correlation of transition Reynolds number with aerodynamic noise levels in a wind tunnel at Mach numbers 2.0-3.0
3. Boundary-Layer Transition
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