Wave excitation in an unsteady boundary layer
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-1833
Reference15 articles.
1. The response of laminar skin friction and heat transfer to fluctuations in the stream velocity
2. The effects of a sound wave on the compressible boundary layer on a flat plate
3. •'Lam, S. H. and Rott, N. "Theory of Linearized Time-Dependent Boundary Layers,"AFOSR Report TN-60-1100, Cornell Univ., 1960.
4. Eigen-Functions of Linearized Unsteady Boundary Layer Equations
5. The unsteady laminar boundary layer on a semi-infinite flat plate due to small fluctuations in the magnitude of the free-stream velocity
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