Extreme shockwave systems in problems of external supersonic aerodynamics-Reference-Cited by-同舟云学术

Extreme shockwave systems in problems of external supersonic aerodynamics

Published:2014-02 Issue:1 Volume:21 Page:15-30
ISSN:0869-8643
Container-title:Thermophysics and Aeromechanics
language:en
Short-container-title:Thermophys. Aeromech.

Author:

Uskov V. N.,Chernyshov M. V.

Publisher

Pleiades Publishing Ltd

Subject

Nuclear and High Energy Physics,Radiation

Link

http://link.springer.com/content/pdf/10.1134/S086986431401003X.pdf

Reference19 articles.

1. G.I. Petrov and E.P. Ukhov, Pressure recovery computation at a passage from the supersonic flight to subsonic one at different systems of planar shocks, Tekhnicheskie zapiski NII-1, 1947, No. 1, P. 1–7.

2. G.I. Petrov, Diffusers for supersonic air breathing engine, Trudy TsIAM, 1950, Issue 169, P. 1–25.

3. G.I. Petrov, Aeromechanics of High Velocities and Space Research: Selected Works, Nauka, Moscow, 1992.

4. K. Oswatitsch, Gas dynamics, Academic Press, New York, 1956.

5. R. Hermann, Supersonic Inlet Diffusers and Introduction to Internal Aerodynamics, Minneapolis-Honeywell Regulator Company Ltd., Minneapolis, 1956.

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