Interference heating due to shock wave impingement on laminar boundary layers
Author:
Affiliation:
1. Northrop Corp., Huntsville, Ala.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1973-678
Reference32 articles.
1. v Boundary-Layer Shock-Wave Interaction", NASA SP-228, October 1969.
2. Haslett, R. A., Kaufman 11, L. G., Romanowski, R. F., and L'rkovitz,El. "Interference Heating Due to Shock Impinscment",AFFDL-TR-72-66, July 1972.
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