A summary of the work performed under NASA grant is presented. More details can be found in the cited references. This grant led to the development of relatively faster aeroelastic analysis methods for predicting flutter and forced response in fans, compressors, and turbines using computational fluid dynamic (CFD) methods. These methods are based on linearized two- and three-dimensional, unsteady, nonlinear aerodynamic equations. During the period of the grant, aeroelastic analysis that includes the effects of uncertainties in the design variables has also been developed.
Aeroelastic Stability and Response of Rotating Structures
2004-01-01
Report
No indication
English
Aeroelastic Stability & Response of Rotating Structures
NTRS | 2001
|Aeroelastic Stability of Rotating Blade
British Library Conference Proceedings | 2012
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