Boundary-layer tables for similar compressible flow
Author:
Affiliation:
1. University of Oklahoma, Norman, Oklahoma
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10240
Reference2 articles.
1. Acceleration and cooling effects in laminar boundary layers - Subsonic, transonic, and supersonic speeds
2. The behaviour of similar solutions in a compressible boundary layer
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