Recent progress in the development of a general purpose unsteady aerodynamic and aeroelastic analysis capability for Advanced Turboprops will be reviewed. An application to a rotor with alternating forward and backward swept blades is described, which illustrates the general 'mistuning' capability of the method.
Aeroelastic effects of alternate blade sweep on advanced propfan rotor
Aeroelastische Wirkung der Wechsel-Blattpfeilung an zukunftsweisenden Propellerturbinen-Drehfluegeln
ASME-Papers ; Dec ; 1-6
1987
6 Seiten, 10 Bilder, 5 Quellen
Conference paper
English
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