Aircraft Conceptual Design Optimization Considering Fidelity Uncertainties-Reference-Cited by-同舟云学术

Aircraft Conceptual Design Optimization Considering Fidelity Uncertainties

Published:2011-09 Issue:5 Volume:48 Page:1602-1612
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Neufeld Daniel¹,Chung Joon²,Behdinian Kamran²

Affiliation:

1. Konkuk University, Seoul 143-701, Republic of Korea

2. Ryerson University, Toronto, Ontario M5B 2K3, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031312

Reference61 articles.

1. Multiconstrained aerodynamic design of business jet by CFD driven optimization tool

2. Takemiya, T. "Aerodynamic Design Applying Automatic Differentiation and Using Robust Variable Fidelity Optimization," Ph.D. Thesis, Georgia Inst. of Technology, Atlanta,GA, 2008.

3. High-Fidelity Computational Optimization for 3-D Flexible Wings: Part I—Simultaneous Aero-Structural Design Optimization (SASDO)

4. Aircraft Conceptual Design Synthesis

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