Experimental and numerical investigation on the supersonic inlet buzz with angle of attack-Reference-Cited by-同舟云学术

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Experimental and numerical investigation on the supersonic inlet buzz with angle of attack

Published:2009 Issue: Volume: Page:1111-1116
ISSN:
Container-title:Shock Waves
language:
Short-container-title:

Author:

Lee H.-J.,Jeung I.-S.

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/978-3-540-85181-3_51.pdf

Reference4 articles.

1. Ferri, A., and Nucci, L. M.: The Origin of Aerodynamic Instability of Supersonic Inlets at Subcritical Conditions, edition (NACA RM L50K30,1951)

2. Dailey, C. L.: Supersonic Diffuser Instability. Ph.D. Thesis, California Institute of Technology, CA (1954)

3. Oswatitsch, K.: Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds, edition (NACA TM-1140, 1948)

4. John ,J . M.: Inlets for Supersonic Missiles, edition (AIAA Education Series, 1990) pp.23-54

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