AIAA-2006-1736 Aeroelastic Analysis of an Airfoil with a Hysteresis Non-Linearity
Robust Flutter Analysis of an Airfoil with Flap Freeplay Uncertainty
Dynamic Pressure Perturbation Method for Flutter Solution: The Mu-Omega Method
Unified Flutter Solution Technique Using Matrix Singularity Indicators
Generalized Mu-Omega Method with Complex Perturbation to Dynamic Pressure