NASA NTRS ยท 19930007371
Aeroelastic stability and response of rotating structures
Abstract
A summary of the work performed during the progress period is presented. Analysis methods for predicting loads and instabilities of wind turbines were developed. Three new areas of research to aid the Advanced Turboprop Project (ATP) were initiated and developed. These three areas of research are aeroelastic analysis methods for cascades including blade and disk flexibility; stall flutter analysis; and computational aeroelasticity.
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Keith, Theo G., Jr.. 1993-01-01. Aeroelastic stability and response of rotating structures. https://ntrs.nasa.gov/citations/19930007371
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