Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration-Reference-Cited by-同舟云学术

Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration

Published:2014-01 Issue:1 Volume:51 Page:144-160
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Kenway Gaetan K. W.¹,Martins Joaquim R. R. A.¹

Affiliation:

1. Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032150

Reference60 articles.

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4. Some Aeroelastic Properties of Swept Wings

5. BrownH. “A Method for the Determination of the Spanwise Load Distribution of a Flexible Swept Wing at Subsonic Speeds,” Defense Technical Information Center, TN-2222, Fort Belvoir, VA, 1951.

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