Continuation Method for Calculation of Transonic Airfoil Flutter Boundaries
- 1 November 1997
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 20 (6) , 1165-1171
- https://doi.org/10.2514/2.4172
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Development of a finite element aeroelastic analysis capabilityJournal of Aircraft, 1996
- Eigenmode analysis in unsteady aerodynamics - Reduced-order modelsAIAA Journal, 1996
- Navier-Stokes computations on flexible advanced transport wings in transonic regimeJournal of Aircraft, 1996
- Nonlinear analysis of airfoil flutter at transonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Hope bifurcation in viscous, low-speed flows about an airfoil with structural couplingComputers & Fluids, 1994
- Static aeroelastic analysis of fighter aircraft using a three-dimensional Navier-Stokes algorithmJournal of Aircraft, 1990
- Unsteady transonic algorithm improvements for realistic aircraft applicationsJournal of Aircraft, 1989
- The Calculation of Hopf Points by a Direct MethodIMA Journal of Numerical Analysis, 1983
- High resolution schemes for hyperbolic conservation lawsJournal of Computational Physics, 1983
- Continuation Methods in Computational Fluid DynamicsPublished by Springer Nature ,1982