Structural optimization for joined-wing synthesis
Authors:
- 1 January 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 33 (1) , 214-223
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
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- Parametric weight evaluation of joined wings by structural optimizationJournal of Aircraft, 1988
- Structural Weight Comparison of a Joined Wing and a Conventional WingJournal of Aircraft, 1982
- V-Wings and Diamond Ring-Wings of Minimum Induced DragJournal of Aircraft, 1972