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Calculation of thermal-fatigue life based on accumulated creep damageCreep rupture data for predicting thermal fatigue cracking of turbine blades or disks
Document ID
19690030008
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Spera, D. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1969
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-5489
E-4950
Report Number: NASA-TN-D-5489
Report Number: E-4950
Accession Number
69N39393
Funding Number(s)
CONTRACT_GRANT: 129-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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