The NASA Lewis aeroelastic research program is focused on unstalled and stalled flutter, forced response, and whirl flutter of turborotors and propfans. The objectives are to understand the physical phenomena of cascade flutter and response including blade mistuning.
Development of aeroelastic analysis methods for turborotors and propfans, including mistuning
1988-05-01
Conference paper
No indication
English
Aeroelastic Analysis Methods for Turbomachines and Propfans
British Library Conference Proceedings | 1993
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