Collaborative study of incipient separation on 53°-swept diamond wing
Author:
Funder
Vehicle Systems Safety Technologies
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference28 articles.
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2. Integrated computational/experimental approach to unmanned combat air vehicle stability and control estimation;Cummings;J. Aircr.,2012
3. A. Hövelmann, F. Knoth, C. Breitsamter, Leading-edge roughness effects on the flow separation onset of the AVT-183 diamond wing, in: AIAA Science and Technology Forum and Exposition (SciTech 2015), AIAA Paper 2015-0063, January 2015.
4. A. Hövelmann, M. Grawunder, C. Breitsamter, Experimental analyses on the flow field characteristics of the AVT-183 diamond wing, in: AIAA Science and Technology Forum and Exposition (SciTech 2015), AIAA Paper 2015-0064, January 2015.
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