Finite volume method for three-dimensional transonic potential flow through turbomachinery blade rows-Reference-Cited by-同舟云学术

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Finite volume method for three-dimensional transonic potential flow through turbomachinery blade rows

Published:1983-06 Issue:2 Volume:4 Page:85-96
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

Reference6 articles.

1. A finite volume method for transonic potential flow equations;Jameson;AIAA Paper No. 77-635,1977

2. A fast conservative algorithm for solving the transonic full potential equation;Holst;AIAA Paper No. 79-1456,1979

3. Calculation of transonic potential flow through turbomachinery blade rows;Soulis;Ph.D. Thesis Cambridge University,1982

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

5. A study of shock waves in three-dimensional transonic flow;Dawes;Ph.D. Thesis Cambridge University,1979

Cited by 1 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. Thin turbomachinery blade design using a finite-volume method;International Journal for Numerical Methods in Engineering;1985-01

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