Interaction between a supersonic boundary layer and acoustic disturbances
Author:
Publisher
Springer Science and Business Media LLC
Subject
Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/BF01090319.pdf
Reference10 articles.
1. G. B. Schubauer and H. K. Skramstad, ?Laminar boundary-layer oscillations and stability of laminar flow,? J. Aeronaut. Sci.,14, No. 2 (1947).
2. H. L. Rogler and E. Reshotko, ?Disturbances in a boundary layer introduced by a flow intensity array of vortices,? SIAM J. Appl. Math.,2, No. 2 (1957).
3. M. V. Markovin, ?On transition experiments at moderate supersonic speeds,? J. Aeronaut. Sci.,24, No. 7 (1957).
4. S. R. Pate and C. J. Schueler, ?Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels,? AIAA J.,7, No, 3 (1969).
5. L. M. Mack, ?On the application of linear stability theory and the problem of supersonic boundary-layer transition,? AIAA J.,13, No. 3 (1975).
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