Aeroelastic and strength optimisation of a large aircraft wing with wing parameter variations-Reference-Cited by-同舟云学术

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Aeroelastic and strength optimisation of a large aircraft wing with wing parameter variations

Published:1998-04-20 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit
language:
Short-container-title:

Author:

Battoo Rupinder¹,de Visser J.²

Affiliation:

1. Cranfield Univ., Bedford, United Kingdom

2. Delft Univ. of Technology, Netherlands

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1821

Reference10 articles.

1. Flutter optimization of large transport aircraft

2. Comparative evaluation of two MDO codes in aircraft wing analysis and optimization

Cited by 3 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. Evolutionary optimization of transonic airfoils for static and dynamic trim performance;Journal of Intelligent Material Systems and Structures;2016-12-06

2. Aeroelastic two-level optimization for preliminary design of wing structures considering robust constraints;Chinese Journal of Aeronautics;2014-04

3. Evolutionary Optimization for Simultaneous Design on Supersonic Flutter and Structural Mass;9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization;2002-09-04

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