A numerical method for calculating steady unsymmetrical supersonic flow past cones-Reference-Cited by-同舟云学术

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A numerical method for calculating steady unsymmetrical supersonic flow past cones

Published:1970-06 Issue:3 Volume:5 Page:463-486
ISSN:0021-9991
Container-title:Journal of Computational Physics
language:en
Short-container-title:Journal of Computational Physics

Author:

Holt Maurice,Ndefo D.Ejike

Publisher

Elsevier BV

Subject

Computer Science Applications,Physics and Astronomy (miscellaneous),Applied Mathematics,Computational Mathematics,Modelling and Simulation,Numerical Analysis

Reference31 articles.

1. On Supersonic Flow Past A Slightly Yawing Cone

2. On Supersonic Flow Past a Slightly Yawing Cone II

3. Tech. Report No. 5;Kopal,1949

4. The Exact Flow Behind a Yawed Conical Shock;Radhakrishnan,1958

Cited by 16 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Telenin’s Method and the Method of Lines;Numerical Methods in Fluid Dynamics;1984

2. The Method of Integral Relations;Numerical Methods in Fluid Dynamics;1984

3. 10. Dimensional Analysis and Model Testing Principles;Fluid Dynamics;1981

4. Experimental investigation of the supersonic flow past a slender cone at high incidence;Journal of Fluid Mechanics;1978-08

5. Symmetrical flow past a double wedge at high subsonic Mach numbers;Journal of Fluid Mechanics;1978-05-15

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