A method of through computation for two- and three-dimensional supersonic flows. I-Reference-Cited by-同舟云学术

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A method of through computation for two- and three-dimensional supersonic flows. I

Published:1972-01 Issue:2 Volume:12 Page:196-221
ISSN:0041-5553
Container-title:USSR Computational Mathematics and Mathematical Physics
language:en
Short-container-title:USSR Computational Mathematics and Mathematical Physics

Author:

Ivanov M.Ya.,Kraiko A.I.,Mikhailov N.V.

Publisher

Elsevier BV

Subject

General Engineering

Reference43 articles.

1. Experience in computing plane and rotationally symmetric supersonic gas flows by the method of characteristics;Katskova,1961

2. Computation of equilibrium gas flows in supersonic nozzles;Katskova,1964

3. Computation of plane and rotationally symmetric supersonic flows in the presence of irreversible processes;Katskova,1964

4. The numerical solution of problems in gas dynamics;Belotserkovskii,1965

5. The method of characteristics for equilibrium flows of an imperfect gas;Naumova,1964

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1. Internal Shocks in Supersonic Flows past the Contours of Optimal Bodies and Nozzles;Fluid Dynamics;2020-11

2. Algorithm for the determination of conditions on the axis of a cylindrical coordinate system in the calculation of 3D viscous jet flows;Technical mechanics;2018-12-27

3. Special Nozzles, Three-Dimensional Flows, Viscosity Effect;Gas Flow in Nozzles;1986

4. Numerical Methods of Studying Nozzle Gas Flows;Gas Flow in Nozzles;1986

5. Steady flow around a plane cascade by an ideal gas;Journal of Applied Mechanics and Technical Physics;1984-11

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