Nonlinear Response Structural Optimization of a Joined Wing Using Equivalent Loads

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Nonlinear Response Structural Optimization of a Joined Wing Using Equivalent Loads

Nonlinear Response Structural Optimization of a Joined Wing Using Equivalent Loads

Kim, Y. I. / Park, G. J. / Kolonay, R. M. / Blair, M. / Canfield, R. A.

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Title :

Nonlinear Response Structural Optimization of a Joined Wing Using Equivalent Loads

Contributors:

Kim, Y. I. (author) / Park, G. J. (author) / Kolonay, R. M. (author) / Blair, M. (author) / Canfield, R. A. (author)

Published in:

AIAA Journal ; 46 , 11 ; 2703-2713

Publication date :

2008-11-01

Size :

11 pages

ISSN :

0001-1452 , 1533-385X

DOI :

https://doi.org/10.2514/1.33428

Type of media :

Article (Journal)

Type of material :

Electronic Resource

Language :

English

Keywords :

Joined Wings , Structural Optimization , Joined Wing Aircraft , Air Force Research Laboratory , Structural Weight , Aerodynamic Performance , Finite Element Analysis , Lift Forces , Wing Root , Allowable Stress

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