Effect of freestream noise on roughness-induced boundary-layer transition for a scramjet inlet
Author:
Affiliation:
1. National Aerospace Lab., Chofu, Japan
2. Purdue Univ., West Lafayette, IN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-284
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3. A. Chpoun;Hypersonicflow in acompressioncomer in 2d and 3d configurations,Paper89-1876,AIAA, June1989.
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