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Dynamic characteristics of an assembly of prop-fan bladesIn contrast to conventional propellers, propfan blades are thin and highly swept-back, thereby giving rise to large bending and twisting deformations and complex vibratory characteristics. Aerodynamic performance depends on the extent of steady state deformation, and the aeroelastic response depends on the vibratory frequency and mode shape. Attention is presently given to the principal results of structural analyses for a five-bladed propfan assembly; these results are compared with test data. The results encompass both steady deformations and vibratory frequencies and mode shapes in a vacuum centrifugal environment.
Document ID
19860048218
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Srinivasan, A. V.
(United Technologies Research Center East Hartford, CT, United States)
Kielb, R. E.
(United Technologies Research Center East Hartford, CT, United States)
Lawrence, C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1986
Publication Information
Publication: ASME, Transactions, Journal of Engineering for Gas Turbines and Power
Volume: 108
ISSN: 0022-0825
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ASME PAPER 85-GT-134
Accession Number
86A32956
Distribution Limits
Public
Copyright
Other

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