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Slow Crack Growth Analysis of Advanced Structural Ceramics Under Combined Loading Conditions: Damage Assessment in Life Prediction TestingSlow crack growth analysis was performed with three different loading histories including constant stress-rate/constant stress-rate testing (Case 1 loading), constant stress/constant stress-rate testing (Case 2 loading), and cyclic stress/constant stress-rate testing (Case 2 loading). Strength degradation due to slow crack growth and/or damage accumulation was determined numerically as a function of percentage of interruption time between the two loading sequences for a given loading history. The numerical solutions were examined with the experimental data determined at elevated temperatures using four different advanced ceramic materials, two silicon nitrides, one silicon carbide and one alumina for the Case 1 loading history, and alumina for the Case 3 loading history. The numerical solutions were in reasonable agreement with the experimental data, indicating that notwithstanding some degree of creep deformation presented for some test materials slow crack growth was a governing mechanism associated with failure for all the test materials.
Document ID
20010061463
Acquisition Source
Glenn Research Center
Document Type
Reprint (Version printed in journal)
Authors
Choi, Sung R.
(Ohio Aerospace Inst. Cleveland, OH United States)
Gyekenyesi, John P.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
August 20, 2013
Publication Date
January 1, 2000
Publication Information
Publication: International Gas Turbine and Aeroengine Congress and Exhibition
Subject Category
Structural Mechanics
Report/Patent Number
ASME-2000-GT-62
Meeting Information
Meeting: International Gas Turbine and Aeroengine Congress and Exhibition
Location: Munich
Country: Germany
Start Date: May 8, 2000
End Date: May 11, 2000
Sponsors: American Society of Mechanical Engineers
Distribution Limits
Public
Copyright
Other

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