Effect of Tripping on Hypersonic Turbulent Boundary-Layer Statistics
Author:
Affiliation:
1. University of Washington, Seattle, Washington 98195
2. Princeton University, Princeton, New Jersey 08544
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055471
Reference47 articles.
1. Effects of slight nose bluntness and roughness on boundary-layer transition in supersonic flows
2. BrinichP. F. “Boundary Layer Transition at Mach 3.12 with and Without Single Roughness Elements,” NACA TN-3267, 1954.
3. Development of second-mode instability in a Mach 6 flat plate boundary layer with two-dimensional roughness
4. Discrete Roughness Transition for Hypersonic Flight Vehicles
5. Effects of Roughness on Hypersonic Boundary-Layer Transition
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