BOUNDARY LAYER TRANSITION- FREESTREAM TURBULENCE AND PRESSURE GRADIENT EFFECTS
Author:
Affiliation:
1. North American Aviation Inc., Downey, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.1784
Reference15 articles.
1. On the aerodynamic heating of blunt bodies
2. Dryden, H. L. "Air flow in the boundary layer near a plate," NACARept.562(1936).
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