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Turbine blade testing methodsTesting procedures which could be used to model test turbine blades are developed. The methods studied were methods which used and extended current modal testing procedures. An acoustical impacting testing method was perfected for testing small turbine blades.
Document ID
19840010133
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:170982
NASA-CR-170982
Report Number: NAS 1.26:170982
Report Number: NASA-CR-170982
Accession Number
84N18201
Funding Number(s)
CONTRACT_GRANT: NAS8-34503
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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