Further Investigation of the Support System Effects and Wing Twist on the NASA Common Research Model-Reference-Cited by-同舟云学术

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Further Investigation of the Support System Effects and Wing Twist on the NASA Common Research Model

Published:2012-06-25 Issue: Volume: Page:
ISSN:
Container-title:30th AIAA Applied Aerodynamics Conference
language:
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Author:

Rivers Melissa¹,Hunter Craig¹,Campbell Richard¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-3209

Reference44 articles.

1. Redeker, G. "DLR-F4 Wing Body Configuration," A Selection of Experimental Test Cases for the Validation of CFD Codes, AGARD Report AR-303, Vol.2, 1994, pp.B4-B1-21.

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