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Development and application of a unified balancing approach with multiple constraintsThe development of a general analytic approach to constrained balancing that is consistent with past influence coefficient methods is described. The approach uses Lagrange multipliers to impose orbit and/or weight constraints; these constraints are combined with the least squares minimization process to provide a set of coupled equations that result in a single solution form for determining correction weights. Proper selection of constraints results in the capability to: (1) balance higher speeds without disturbing previously balanced modes, thru the use of modal trial weight sets; (2) balance off-critical speeds; and (3) balance decoupled modes by use of a single balance plane. If no constraints are imposed, this solution form reduces to the general weighted least squares influence coefficient method. A test facility used to examine the use of the general constrained balancing procedure and application of modal trial weight ratios is also described.
Document ID
19850018580
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zorzi, E. S.
(Mechanical Technology, Inc. Latham, NY, United States)
Lee, C. C.
(Mechanical Technology, Inc. Latham, NY, United States)
Giordano, J. C.
(Mechanical Technology, Inc. Latham, NY, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: NASA. Marshall Space Flight Center Advan. High Pressure O2(H2 Technol.
Subject Category
Structural Mechanics
Accession Number
85N26891
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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