Progress toward using sensitivity derivatives in a high-fidelity aeroelastic analysis of a supersonic transport-Reference-Cited by-同舟云学术

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Progress toward using sensitivity derivatives in a high-fidelity aeroelastic analysis of a supersonic transport

Published:1998-08-22 Issue: Volume: Page:
ISSN:
Container-title:7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
language:
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Author:

Giunta Anthony¹,Sobieszczanski-Sobieski Jaroslaw¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-4763

Reference32 articles.

1. Direct calculation of aerodynamic force derivatives - A sensitivity-equation approach

2. Haftka, R. T. and Gurdal, Z. Elements of Structural Optimization, pp.211-219,305-316,Kluwer, Boston, MA, 3rd edition (1993).

Cited by 18 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. Numerical sensitivity analysis for aerodynamic optimization: A survey of approaches;Computers & Fluids;2010-03

2. Multidisciplinary Code Coupling for Analysis and Optimization of Aeroelastic Systems;Journal of Aircraft;2009-11

3. Sensitivity Analysis of a Strongly Coupled Aero-Structural System Using Direct and Adjoint Methods;12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2008-06-14

4. Aeroelastic design optimization for laminar and turbulent flows;Computer Methods in Applied Mechanics and Engineering;2008-03

5. Sensitivity analysis of a strongly coupled aero-structural system using the discrete direct and adjoint methods;European Journal of Computational Mechanics;2008-01

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