Two-component LDV investigation of three-dimensional shock/turbulentboundary-layer interactions
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California
2. University of California, Berkeley, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9850
Reference6 articles.
1. Brown, J. D. "Two-Component LDV Investigation of Shock-Related Turbulent Boundary Layer Separation with Increasing Three Dimensionality," Ph.D. Thesis,University of California, Berkeley, 1986.
2. The prediction of laminarization with a two-equation model of turbulence
3. 4MacCormack, R. W. "Numerical Solution of the Interaction of a Shock Wave with a Laminar Boundary Layer," Lecture Notes in Physics, Vol.8, 1972, Springer-Verlag, Berlin, pp.151-163.
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