MAVRIC flutter model transonic limit cycle oscillation test-Reference-Cited by-同舟云学术

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MAVRIC flutter model transonic limit cycle oscillation test

Published:2001-06-11 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Edwards John¹,Schuster David¹,Spain Charles¹,Keller Donald¹,Moses Robert¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1291

Reference21 articles.

1. Limit Cycle Oscillation Characteristics of Fighter Aircraft

2. Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores

3. Cunningham,A.M.Jr.:AGeneric Nonlinear Aeroelastic MethodWithSemi-EmpiricalNonlinear UnsteadyAerodynamics,Volume I.Technical Discussion.AFRL-VA-WP-TR-1999-3014, February 1999.

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2. Nonlinear Aeroelasticity;A Modern Course in Aeroelasticity;2021-10-16

3. Experiments on transonic limit-cycle-flutter of a flexible swept wing;Journal of Fluids and Structures;2019-01

4. Computational Study of Transonic Limit Cycle Oscillation Phenomenon on F-16 Fighter Aircraft;Journal of Aircraft;2017-03

5. A review on non-linear aeroelasticity of high aspect-ratio wings;Progress in Aerospace Sciences;2017-02

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