Flutter of a Swept Aircraft Wing with a Powered Engine

Author:

Mazidi A.12,Fazelzadeh S. A.12

Affiliation:

1. Ph.D. Candidate, Dept. of Mechanical Engineering, Shiraz Univ., Shiraz, Iran.

2. Associate Professor, Dept. of Mechanical Engineering, Shiraz Univ., Shiraz, Iran (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Cited by 32 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. Engine Placement Effects on the Flutter of a Medium-Range Box-Wing Aircraft;Journal of Aerospace Engineering;2023-07

2. Flutter instability boundary determination of composite wings using adaptive support vector machines and optimization;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2023-03

3. Flutter Analysis of a 3-D Box Wing with Distributed Electric Propulsion;Sustainable Aviation;2023

4. Analysis of flutter characteristics of swept wing;Seventh International Conference on Electromechanical Control Technology and Transportation (ICECTT 2022);2022-11-23

5. Flutter Analysis of a 3D Box-Wing Aircraft Configuration;International Journal of Structural Stability and Dynamics;2021-12-29

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