Transonic Limit Cycle Oscillation Analysis Using Aerodynamic Describing Functions and Superposition Principle-Reference-Cited by-同舟云学术

Transonic Limit Cycle Oscillation Analysis Using Aerodynamic Describing Functions and Superposition Principle

Published:2014-07 Issue:7 Volume:52 Page:1393-1403
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

He Shun¹,Yang Zhichun¹,Gu Yingsong¹

Affiliation:

1. Institute of Structural Dynamics and Control, School of Aeronautics, 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.J052559

Reference24 articles.

1. IsogaiK. “Numerical Study of Transonic Flutter of a Two-Dimensional Airfoil,” National Aerospace Lab. TR-617T, Chofu, Tokyo, Japan, July 1980.

2. Wing flutter boundary prediction using unsteady Euler aerodynamic method

3. Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations

4. Fully-implicit time-marching aeroelastic solutions

5. Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method

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