Experimental Mixing Profiles of a Mach 2.6 Free Jet
Author:
Affiliation:
1. Department of Aeronautical Engineering, Princeton University, Princeton, N.J.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.7893
Reference11 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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