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Steady-state stress relaxation analysis of turbine blade cooling designsSteady state stress relaxation analysis of turbine blade cooling designs
Document ID
19690019943
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Kaufman, A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-5282
Accession Number
69N29321
Funding Number(s)
CONTRACT_GRANT: 720-03-00-74-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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