A finite volume method for two-dimensional transonic potential flow through turbomachinery blade rows-Reference-Cited by-同舟云学术

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A finite volume method for two-dimensional transonic potential flow through turbomachinery blade rows

Published:1983-12 Issue:4 Volume:4 Page:229-237
ISSN:0142-727X
Container-title:International Journal of Heat and Fluid Flow
language:en
Short-container-title:International Journal of Heat and Fluid Flow

Author:

Soulis J.V.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference12 articles.

1. Artificial compressibility methods for numerical solution of transonic full potential equation;Hafez;AIAA Paper No 78-1148,1971

2. Numerical technique for the calculation of transonic flow in turbomachinery cascades;Gopalakrishnan;ASME Paper No 71-GT-42,1971

3. A time marching method for two and three dimensional blade to blade flows;Denton;Aeronautical Research Council R&M, 3775,1975

4. The calculation of two dimensional compressible potential flow in cascades using finite are techniques;Caspar;AIAA 17th Aerospace New Orleans,1979

5. Transonic flow computations in cascades using a finite-element method;Acay;ASME Paper No. 81-GT-4,1981

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. Torsional analysis of flanged concrete elements with tension softening;Computers & Structures;1995-01

2. Two-dimensional unsaturated flow in irregularly shaped regions using a finite volume method;Transport in Porous Media;1991-02

3. A numerical method for torsional analysis of structural elements;Computers & Structures;1990-01

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