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Correlation of creep rate with microstructural changes during high temperature creepCreep tests were conducted on Haynes 188 cobalt-base alloy and alpha titanium. The tests on Haynes 188 were conducted at 1600 F and 1800 F for stresses from 3 to 20 ksi, and the as-received, mill-annealed results were compared to specimens given 5%, 10%, and 15% room temperature prestrains and then annealed one hour at 1800 F. The tests on alpha titanium were performed at 7,250 and 10,000 psi at 500 C. One creep test was done at 527 C and 10,000 psi to provide information on kinetics. Results for annealed titanium were compared to specimens given 10% and 20% room temperature prestrains followed by 100 hours recovery at 550 C. Electron microscopy was used to relate dislocation and precipitate structure to the creep behavior of the two materials. The results on Haynes 188 alloy reveal that the time to reach 0.5% creep strain at 1600 F increases with increasing prestrain for exposure times less than 1,000 hours, the increase at 15% prestrain being more than a factor of ten.
Document ID
19770025341
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Young, C. T.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Sommers, B. R.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Lytton, J. L.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1977
Subject Category
Metallic Materials
Report/Patent Number
NASA-CR-145220
Report Number: NASA-CR-145220
Accession Number
77N32285
Funding Number(s)
CONTRACT_GRANT: NGR-47-004-108
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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