SHOCK-INDUCED BOUNDARY LAYER SEPARATION IN OVER-EXPANDED CONICAL EXHAUST NOZZLES
Author:
Affiliation:
1. Technion-Israel Institute of Technology, Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.1598
Reference21 articles.
1. Shapiro, A. F., The Dynamics and Thermodynamics of Compressible Fluid Flow (Ronald Press, New York, 1953), Vol.I, pp.140-141.
2. Tecnical Notes
3. 4McKenney, J. D., Ae. E. Thesis, Calif. Inst. Tech. (1949).
4. Editors
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