Multidisciplinary Design Optimization of Subsonic Strut-Braced Wing Aircraft-Reference-Cited by-同舟云学术

Multidisciplinary Design Optimization of Subsonic Strut-Braced Wing Aircraft

Published:2014-01-10 Issue: Volume: Page:
ISSN:
Container-title:52nd Aerospace Sciences Meeting
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Author:

Gupta Rikin¹,Mallik Wrik¹,Kapania Rakesh K.¹,Schetz Joseph A.¹

Affiliation:

1. Virginia Polytechnic Institute and State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0186

Reference15 articles.

1. U.S. Department of Defense, "Annual Fuel Consumption," http://www.defense.gov/news/newsarticle.aspx?id=117084.

2. Pfenninger, W. "Laminar Flow Control Laminarization," AGARD Report 654, "Special Course on Concepts for Drag Reduction" , 1977, Summarized from the report "Some thoughts on the design of large global rangeLFCtransport airplanes," Jan., 1976.

3. Multidisciplinary Design Optimization of a transonic strut-braced wing aircraft

4. Conceptual Design Studies of a Strut-Braced Wing Transonic Transport

5. Transport Weight Reduction Through MDO: The Strut-Braced Wing Transonic Transport

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