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Vibrational Effects of Turbopump Housing FlexibilityMethods of computer simulation of turbopump vibrations described in report. For aircraft and aerospace service, high-speed, high-performance turbomachinery should be as light in weight as possible. Certain amount of mass needed in turbomachine housing for stiffness. Report addresses question of how much extra weight is necessary. Analyses shows under certain conditions, flexible housing more stable than rigid one.
Document ID
19850000552
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Fenwick, J. R.
(Rockwell International Corp.)
Tarn, R. B.
(Rockwell International Corp.)
Date Acquired
August 12, 2013
Publication Date
March 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 9
Issue: 4
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
MFS-27083
Accession Number
85B10552
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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