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
01.01.2010
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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
|