The application of finite difference methods to the supersonic near wake
Author:
Affiliation:
1. Princeton University, Princeton, N.J.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1972-115
Reference11 articles.
1. Burger, S. A., L,minar Wakes, Amepican Elsevier, New YoPk, 1971.
2. Solution of the time-dependent Navier-Stokes equations for the flow around a circular cylinder.
3. S. Ross, B. B. "An Investigation of the Numer,ical and Physical AspE'Cts of a Finite-Difference M:xlelof the laminar Supersonic Near Wake", Ph.D. Thesis,Princeton University, 1971.
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. Engineering Model for Re-entry Vehicle Turbulent Wakes;Journal of Spacecraft and Rockets;1980-03
2. An engineering model for reentry vehicle turbulent wakes - Applications to electron density prediction and decelerator performance;17th Aerospace Sciences Meeting;1979-01-15
3. The application of finite difference methods to the supersonic near wake;10th Aerospace Sciences Meeting;1972-01-17
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