Bilevel Programming Weight Minimization of Composite Flying-Wing Aircraft with Curvilinear Spars and Ribs-Reference-Cited by-同舟云学术

Bilevel Programming Weight Minimization of Composite Flying-Wing Aircraft with Curvilinear Spars and Ribs

Published:2019-06 Issue:6 Volume:57 Page:2594-2608
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Zhao Wei¹,Kapania Rakesh K.¹

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

Funder

National Aeronautics and Space Administration

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057892

Reference44 articles.

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4. Aeroelastic tailoring - Theory, practice, and promise

5. JutteC.StanfordB. K. “Aeroelastic Tailoring of Transport Aircraft Wings: State-of-the-Art and Potential Enabling Technologies,” NASA TM-2014-218252, 2014.

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