Direct harmonic linear Navier-Stokes methods for efficient simulation of wave packets
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-784
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3. The unsteady laminar boundary layer on a semi-infinite flat plate due to small fluctuations in the magnitude of the free-stream velocity
4. Dagenhart,J.R., Saric,W.S.,Mousseux,M.C.,and Stack,J.P. "Crossflow-Vortex Instability and Transition ona 45-Degree SweptWing,"AIAA Paper 89-1892,1989.
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