High Efficient Numerical Method for Limit Cycle Flutter Analysis Based on Nonlinear Aerodynamic Reduced Order Model Reduced Order Model
51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
2010-01-01
Conference paper
Electronic Resource
English
Nonlinear Aerodynamic Reduced-Order Model for Limit-Cycle Oscillation and Flutter
Online Contents | 2016
|Nonlinear Aerodynamic Reduced-Order Model for Limit-Cycle Oscillation and Flutter
Online Contents | 2016
|