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Testing And Analysis Of Rubbing Of Turbine-Blade TipsUnique combination of established techniques of experimentation and theoretical analysis devised to study stresses induced in turbine blades by intermittent or periodic rubbing of tips of blades in turbine housings. Rubbing is inevitable consequence of modern high-speed, high-efficiency turbine designs, which call for blade-tip clearances as small as possible. Necessary to quantify stresses caused by rubbing in order to predict fatigue lives of blades. Testing apparatus simulates blade-tip rubbing and measures dynamic responses of blades.
Document ID
19950070337
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Davis, Gary A.
(Rockwell International Corp.)
Clough, Ray C.
(Rockwell International Corp.)
Date Acquired
August 16, 2013
Publication Date
October 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 10
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
MFS-29981
Report Number: MFS-29981
ISSN: 0145-319X
Accession Number
95B10516
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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