Design Optimization of Vortex Generators for a Junction Vortex of Wing-Body Configuration by Discrete Adjoint Approach-Reference-Cited by-同舟云学术

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Design Optimization of Vortex Generators for a Junction Vortex of Wing-Body Configuration by Discrete Adjoint Approach

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Yi JunSok¹,Kim Chongam¹

Affiliation:

1. Seoul National University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-634

Reference36 articles.

1. 1Redeker, G. "A Selection of Experimental Test Cases for the Validation of CFD Codes, DLR-F4 Wing Body Configuration,"AGARD AdvisoryReport,AGARD Report AR-303, B-4, Aug. 1994.

2. Investigations of propulsion integration interference effects on a transport aircraft configuration

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