Boundary-layer transition detection and structure identification through surface shear-stress measurements
Author:
Affiliation:
1. Arizona State Univ., Tempe
2. Clarkson Univ., Potsdam, NY
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-782
Reference15 articles.
1. The Proper Orthogonal Decomposition in the Analysis of Turbulent Flows
2. Carillo, R. B. (1996) Distributed-Roughness Effects on Stability and Transition in Swept-Wing Boundary Layers. M.S. thesis,Arizona StateUniversity.
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