A summary of the work performed under NASA grant NCC3-605 is presented. More details can be found in the cited references. This grant led to the development of relatively faster aeroelastic analyses methods for predicting flutter and forced response in fans, compressors, and turbines using computational fluid dynamic (CFD) methods.
Aeroelastic Stability & Response of Rotating Structures
01.03.2001
Report
Keine Angabe
Englisch
Aeroelastic Stability of Rotating Blade
British Library Conference Proceedings | 2012
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