Towards the Use of CFD to Improve and Validate the Wall Correction Methodology at the NRC 1.5 m Trisonic Wind Tunnel-Reference-Cited by-同舟云学术

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Towards the Use of CFD to Improve and Validate the Wall Correction Methodology at the NRC 1.5 m Trisonic Wind Tunnel

Published:2016-06-10 Issue: Volume: Page:
ISSN:
Container-title:32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
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Author:

Toledano Alvaro¹,Weiss Julien¹,Morency François¹,Broughton Cabot²,Benmeddour Ali²

Affiliation:

1. University of Québec

2. National Research Council Canada

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3497

Reference21 articles.

1. 1Mokry, M. "Subsonic Wall Interference Corrections for Half-Model Tests using Sparse Wall Pressure Data," Aeronautical Report LR-616, NRC No. 25132, National Research Council Canada, 1985.

2. Doublet-panel method for half-model wind-tunnel corrections

3. 3Mokry, M. "Subsonic Wall Corrections in the IAR 1.5 m Wind Tunnel," Laboratory Report LR-AL-2006-0056, National Research Council Canada, 2006.

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. Improvement of Wall-Corrections at the National Research Council’s Trisonic Wind Tunnel;Journal of Aircraft;2019-11

2. Study of the Subsonic Wall Interference in Stall of the NASA CRM at the NRC 1.5 m Trisonic Wind Tunnel;33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2017-06-02

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