Suppression of shock wave oscillations on a blunt cone-cylinder-Reference-Cited by-同舟云学术

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Suppression of shock wave oscillations on a blunt cone-cylinder

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
language:
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Author:

Kamaraj V.¹,Stanewsky E.²,Kamaraj V.¹,Stanewsky E.²

Affiliation:

1. National Aerospace Labs., Bangalore, India

2. DLR, Inst. fuer Stroemungsmechanik, Goettingen, Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-299

Reference21 articles.

1. Bahi.L., RossJ.M., and Nagamatsu,H.T. "Passive shock wave/boundary layer control for transonic airfoil drag reduction, "AIAA Paper 83-0137, Jan.1983.

2. Nagamatsu, H.T., Dyer,R., and Ficarra.R.V. "Supercritical airfoil drag reduction bypassive shock wave/ boundary layer control in the Mach number range 0.75 to 0.90, "AIAAPaper 85-0207,Jan.1985.

3. Effects of suction on shock/boundary-layer interaction and shock-induced separation

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