The strongly implicit procedure applied to the flow field of transonic turbine cascades
Author:
Affiliation:
1. USAF, Institute of Technology, Wright-Patterson AFB, Ohio
2. Lockheed-Georgia Co., Marietta, Ga.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-211
Reference14 articles.
1. Second-Order-Accurate Calculation of Transonic Flow over Turbomachinery Cascades
2. Investigation of transonic flow in a cascade using an adaptive mesh
3. Lecture Notes in Fluid Mecl;LlLuer F.,1975
4. stems f-r Solution of Partial Differential Equa-EYions on Fields Containing Any Number of Arbitrary rwc -niln*ns iona? Bodies,'3 NASA CR-2729. J, 1 1977.
Cited by 2 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. Transonic flow computations using nonlinear potential methods;Progress in Aerospace Sciences;2000-01
2. Analysis of artificial dissipation models for the transonic full-potential equation;AIAA Journal;1988-10
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