Hypersonic Boundary-Layer Instabilities due to Near-Critical Roughness
Author:
Affiliation:
1. School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana 47097-1282
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A32554
Reference47 articles.
1. Transition Issues for Atmospheric Entry
2. Effects of Roughness on Hypersonic Boundary-Layer Transition
3. SmithA. M. O.GamberoniN. “Transition, Pressure Gradient and Stability Theory,” Douglas Aircraft Co. Rept. ES-26388, Aug. 1956.
4. The eN Method for Transition Prediction. Historical Review of Work at TU Delft
5. Linear Stability Theory Applied to Boundary Layers
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