Continuation Method for Calculation of Transonic Airfoil Flutter Boundaries
Author:
Affiliation:
1. U.S. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433-7765
2. U.S. Air Force Wright Laboratory, Wright–Patterson Air Force Base, Ohio 45433-7913
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.4172
Reference26 articles.
1. Nonlinear analysis of airfoil flutter at transonic speeds
2. Hopf-bifurcation analysis of airfoil flutter at transonic speeds
3. Morton, S. A. “Nonlinear Analysis of Airfoil Flutter at Transonic Speeds,” Ph.D. Thesis, U.S. Air Force Inst. of Technology,Wright-Patterson AFB,OH, May 1996.
4. Unsteady transonic algorithm improvements for realistic aircraft applications
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