The optimum airfoils at low angles of attack in a supersonic gas flow-Reference-Cited by-同舟云学术

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The optimum airfoils at low angles of attack in a supersonic gas flow

Published:1997-01 Issue:1 Volume:61 Page:83-91
ISSN:0021-8928
Container-title:Journal of Applied Mathematics and Mechanics
language:en
Short-container-title:Journal of Applied Mathematics and Mechanics

Author:

Zubov V.I

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials,Modeling and Simulation

Reference8 articles.

1. The optimum supersonic airfoil of specified thickness;Zubov;Izv. Akad. Nauk SSSR. MZhG,1976

2. A general method for the determination of best supersonic rocket nozzles;Guderley,1962

3. Optimal problems of gas dynamics;Sirazetdinov;Izv. Vuzov. Ser. Aviats. Tekh.,1963

4. Variational problems of the gas dynamics of non-equilibrium and equilibrium flows;Kraiko;Prikl. Mat. Mekh.,1964

5. The solution of variational problems of supersonic gas dynamics;Kraiko;Prikl. Mat. Mekh.,1966

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