Finite difference computation for transonic steady potential flows-Reference-Cited by-同舟云学术

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Finite difference computation for transonic steady potential flows

Published:1981-07 Issue:2 Volume:27 Page:129-138
ISSN:0045-7825
Container-title:Computer Methods in Applied Mechanics and Engineering
language:en
Short-container-title:Computer Methods in Applied Mechanics and Engineering

Author:

Luo S.J.,Zheng Y.W.,Qian H.,Wang D.Q.

Publisher

Elsevier BV

Subject

Computer Science Applications,General Physics and Astronomy,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference4 articles.

1. Contribution to methods for calculating the flow about thin lifting wings at transonic speeds—Analytic expressions for far field;Klunker;NASA TND-6530,1970

2. Calculation of plane steady transonic flows;Murman;AIAA J.,1971

3. Transonic load characteristics of 3%-Thick 60° delta-wing-body combination;Swihart;NASA TN D-830,1961

4. Force and pressure measurements at transonic speed for several bodies having elliptical cross sections;McDevitt;NACA TN 4362,1958

Cited by 3 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. Computation of transonic aerodynamically compensating pilot tube;Journal of Aircraft;1988-06

2. Computation of transonic aerodynamically compensating pitot tube;5th Applied Aerodynamics Conference;1987-08-17

3. Finite difference computation of pressure and wave-drag of slender bodies of revolution at transonic speeds with zero-lift;Eighth International Conference on Numerical Methods in Fluid Dynamics;1982

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