Hopf Bifurcation Calculations for a Symmetric Airfoil in Transonic Flow-Reference-Cited by-同舟云学术

Hopf Bifurcation Calculations for a Symmetric Airfoil in Transonic Flow

Published:2004-05 Issue:5 Volume:42 Page:883-892
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Badcock K. J.¹,Woodgate M. A.¹,Richards B. E.¹

Affiliation:

1. University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.9584

Reference22 articles.

1. 1Goura, G. S. L. "Time Marching Analysis of Flutter Using Computational Fluid Dynamics," Ph.D. Dissertation, Dept. of Aerospace Engineering,Univ. of Glasgow, Glasgow, Scotland, U.K.Nov. 2001.

2. Higher-Order Subiteration-Free Staggered Algorithm for Nonlinear Transient Aeroelastic Problems

3. 3Djayapertapa, L. "A Computational Method for Coupled Aerodynamic-Structural Calculations in Unsteady Transonic Flow with Active Control Study," Ph.D. Dissertation, Dept. of Aerospace Engineering,Univ. of Bristol, Bristol, England, U.K.Nov. 2000.

4. Application of a three-field nonlinear fluid–structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter

5. Nonlinear simulation of F-16 aeroelastic instability

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