Parametric weight evaluation of joined wings by structural optimization
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California
2. ACA Industries, Inc., Torrance, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45714
Reference11 articles.
1. The joined wing - An overview
2. 2Fairchild, M. P. "Structural Weight Comparison of a Joined Wing and a Conventional Wing," M.S. Thesis,Univ. of Texas, Arlington, TX, May 1980.
3. Structural Weight Comparison of a Joined Wing and a Conventional Wing
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