Modeling supersonic jet screech - Differential entrainment and amplitude effects
Author:
Affiliation:
1. McDonnell Douglas Corp., Saint Louis, MO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-916
Reference64 articles.
1. Bertolotti, F. P. (1990), "Linear and Nonlinear Stability of Boundary Layers with Streamwise Varying Properties", Ph.D. Thesis,The Ohio State University.
2. LXXIII.The plane jet
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