Bilevel Optimization Strategy for Aircraft Wing Design Using Parallel Computing-Reference-Cited by-同舟云学术

Bilevel Optimization Strategy for Aircraft Wing Design Using Parallel Computing

Published:2014-08 Issue:8 Volume:52 Page:1770-1783
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Elham Ali¹,van Tooren Michel J. L.²,Sobieszczanski-Sobieski Jaroslaw³

Affiliation:

1. Faculty of Aerospace Engineering, Delft University of Technology, 2629 HS Delft, The Netherlands

2. Ronald E. McNair Center for Aerospace Innovation and Research, University of South Carolina, Columbia, South Carolina 29201

3. NASA Langley Research Center, Hampton, Virginia 23601

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052696

Reference44 articles.

1. RegisA. L. D.de MattosB. S.da Mota GirardiR. “Wing Structural Weight Evolution with the Cruise Mach Number of a Commercial Transport Aircraft,” AIAA Paper 2004-5192, Aug. 2004.

2. High-Fidelity Aerostructural Design Optimization of a Supersonic Business Jet

3. Multifidelity, Multistrategy, and Multidisciplinary Design Optimization Environment

4. Computational Approaches for Aerospace Design

5. also AIAA Paper 2010-2914, 2010, pp. 1–21.

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