Aeroelastic analysis of high aspect ratio wing in subsonic flow-Reference-Cited by-同舟云学术

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Aeroelastic analysis of high aspect ratio wing in subsonic flow

Published:2013-01 Issue: Volume: Page:
ISSN:
Container-title:Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)
language:
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Author:

Ahmad K.,Wuzhigang W.,Rahman H.

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/6507009/6512107/06512157.pdf?arnumber=6512157

Cited by 4 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. Limit cycle oscillation prediction based on Finite Element-Modal approach;Archive of Mechanical Engineering;2018-11-05

2. Failure analysis of high aspect ratio flexible wing aeroelastic loading;AIP Conference Proceedings;2018

3. Identification of nonlinear aeroelastic system using fuzzy wavelet neural network;Neurocomputing;2016-11

4. FE-Modal Approach to Model Geometric Nonlinearities of High Aspect Ratio Wing;Applied Mechanics and Materials;2013-08

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