New Improved g Method for Flutter Solution-Reference-Cited by-同舟云学术

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New Improved g Method for Flutter Solution

Published:2009-11 Issue:6 Volume:46 Page:2184-2186
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Ju Qiu¹,Qin Sun¹

Affiliation:

1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.46328

Reference2 articles.

1. Damping Perturbation Method for Flutter Solution: The g-Method

2. Patil, M. J. "Nonlinear Aeroelastic Analysis, Flight Dynamics, and Control of a Complete Aircraft", Ph.D. Dissertation,School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA, 1999.

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1. Verification and Validation of Supersonic Flutter of Rudder Model for Experiment;Optimization Problems in Engineering [Working Title];2021-06-17

2. A generalized eigenvalue solution to the flutter stability problem with true damping: The p-L method;Journal of Fluids and Structures;2021-05

3. Robust active suppression for body-freedom flutter of a flying-wing unmanned aerial vehicle;Journal of the Franklin Institute;2021-03

4. New Mechanism of the Aeroelastic Divergence Onset;AIAA Journal;2020-06

5. Large Amplitude Limit Cycle Oscillations of Fully Coupled Fluid-Structure Interactions;2018 Fluid Dynamics Conference;2018-06-24

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