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Methods for Predicting Thermal Stress Cracking in Turbine Stator or Rotor Blades Summary ReportTest rig for predicting thermal stress cracking in turbine stator or rotor blades
Document ID
19670026021
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
O L Stewart (Pratt and Whitney Aircraft East Hartford, CT, United States)
W H Vogel (Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
August 3, 2013
Publication Date
July 10, 1967
Subject Category
Structural Mechanics
Report/Patent Number
Report Number: NASA-CR-54636
Report Number: PWA-3142
NASA-CR-54636
PWA-3142
Accession Number
67N35350
Funding Number(s)
CONTRACT_GRANT: NAS3-7909
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CRACK
THERMAL STRESS
TURBINE BLADE
TEST STAND

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