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An efficient constraint to account for mistuning effects in the optimal design of engine rotorsBlade-to-blade differences in structural properties, unavoidable in practice due to manufacturing tolerances, can have significant influence on the vibratory response of engine rotor blade. Accounting for these differences, also known as mistuning, in design and in optimization procedures is generally not possible. This note presents an easily calculated constraint that can be used in design and optimization procedures to control the sensitivity of final designs to mistuning.
Document ID
19930036283
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murthy, Durbha V.
(Toledo Univ.; NASA, Lewis Research Center Cleveland, OH, United States)
Pierre, Christophe
(NASA Lewis Research Center Cleveland, OH, United States)
Ottarsson, Gisli
(Michigan Univ. Ann Arbor, United States)
Date Acquired
August 15, 2013
Publication Date
September 1, 1992
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 92-4711
Accession Number
93A20280
Distribution Limits
Public
Copyright
Other

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