Numerical prediction of the reflection plate boundary layer effects on half plane model in wind tunnel-Reference-Cited by-同舟云学术

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Numerical prediction of the reflection plate boundary layer effects on half plane model in wind tunnel

Published:2000-06-19 Issue: Volume: Page:
ISSN:
Container-title:21st Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Zhang F.¹,Khalid M.¹,Xu H.¹,Ball N.¹

Affiliation:

1. NRC of Canada, Inst. for Aerospace Research, Ottawa

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-2376

Reference5 articles.

1. Archie F.K. Yeung, "Half-Model Testing and its Data Accuracy requirements," Technical Report in JAR. June 1998.

2. Kumar, S. "CFO Study of Sting Effect - Stage I," Technical Report in !AR, Sep. 1999.

3. J. Su, "Numerical Analysis of the Aerodynamics of the Aurora Aircraft by an Inviscid/Viscous Interaction Method," Technical Report in JAR,Aug. 1999.

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. A CFD Based Study of UCAV 1303 Model;23rd AIAA Applied Aerodynamics Conference;2005-06-06

2. Investigation of propeller effects on the Aurora aircraft;19th AIAA Applied Aerodynamics Conference;2001-06-11

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