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Slow Crack Growth Behavior and Life/Reliability Analysis of 96 wt % Alumina at Ambient Temperature With Various Specimen/Loading ConfigurationsExtensive constant stress-rate testing for 96 wt % alumina was conducted in room-temperature distilled water using four different specimen/loading configurations: rectangular beam test specimens under four-point uniaxial flexure, square plate test specimens in ring-on-ring biaxial flexure, square plate test specimens in ball-on-ring biaxial flexure, and dog-boned tensile test specimens in pure tension. The slow crack growth (SCG) parameter n was almost independent of specimen/loading configurations, in either four-point uniaxial flexure, ring-on-ring biaxial flexure, ball-on-ring biaxial flexure, or pure tension, ranging from n = 35 to 47 with an average value of n = 41.1 +/- 4.5. The prediction of fatigue strength/reliability based on the four-point uniaxial flexure data by using the CARES/Life design code as well as a simple PIA model was in good agreement with both the ring-on-ring biaxial and the ball-on-ring biaxial flexure data. A poor prediction using the PIA model was observed for the dog-boned tensile test specimens, presumably due to different flaw population involved in the tensile test specimens.
Document ID
20000085867
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Choi, Sung R.
(NASA Glenn Research Center Cleveland, OH United States)
Powers, Lynn M.
(NASA Glenn Research Center Cleveland, OH United States)
Nemeth, Noel N.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2000
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.16:210206
E-12325
NASA/TM-2000-210206
Report Number: NAS 1.16:210206
Report Number: E-12325
Report Number: NASA/TM-2000-210206
Funding Number(s)
PROJECT: RTOP 505-23-1B
CONTRACT_GRANT: DE-AC05-84OR-21400
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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