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Influence of Model Complexity and Aeroelastic Constraints on Multidisciplinary Optimization of Wings

  • Published:1998-09 Issue:5 Volume:35 Page:784-790
  • ISSN:0021-8669
  • Container-title:Journal of Aircraft
  • language:en
  • Short-container-title:Journal of Aircraft

Author:

Bishop Jonathan A.1,Eastep Franklin E.2,Striz Alfred G.3,Venkayya Vipperla B.4

Affiliation:

1. U.S. Air Force Research Laboratory, Kirtland Air Force Base, New Mexico 87117-5776

2. University of Dayton, Dayton, Ohio 45469-0027

3. University of Oklahoma, Norman, Oklahoma 73019-0601

4. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7542

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Multiobjective optimization of an aircraft wing design with respect to structural and aeroelastic characteristics using neural network metamodel;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2018-01

2. Optimal Scheduling of Control Surfaces Flexible Wings to Reduce Induced Drag;Journal of Aircraft;2006-11

3. Induced Drag Minimization of a Free Flying Flexible Vehicle Using Trailing Edge Control Surfaces;11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2006-09-06

4. Roadmap for Moderate Fidelity Conceptual Design with Multilevel Analysis and MDO;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05

5. Optimal Scheduling of Control Surfaces on a Flexible Wing to Reduce Induced Drag;10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2004-08-30
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