Boundary-Layer Transition with Gas Injection
Author:
Affiliation:
1. Rosemount Aeronautical Laboratories, University of Minnesota, Minneapolis, Minn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.7892
Reference4 articles.
1. Barron, J. R., The Binary Mixture Boundary Layer Associated with Mass Transfer Cooling at High Speeds, M I T Tech. Report 160, 1956.
2. Boundary-Layer Transition with Gas Injection
3. Calculation of the Stability of the Laminar Boundary Layer in a Compressible Fluid on a Flat Plate with Heat Transfer
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