Flutter Equation as a Piecewise Quadratic Eigenvalue Problem

Author:

Eller David1

Affiliation:

1. Royal Institute of Technology, SE-100 44 Stockholm, Sweden

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 6 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. A semi-analytical approach for flutter analysis of a high-aspect-ratio wing;The Aeronautical Journal;2020-08-07

2. Semi-Analytical Flutter Analysis of a Light UAV Wing;2020 17th International Bhurban Conference on Applied Sciences and Technology (IBCAST);2020-01

3. On Tracking Aeroelastic Modes in Stability Analysis Using Left and Right Eigenvectors;AIAA Journal;2019-10

4. A Mode Tracking Method in Aeroelastic Stability Analysis Using Left Eigenvectors;2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2018-01-07

5. Aeroelastic flutter analysis considering modeling uncertainties;Journal of Fluids and Structures;2017-10

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