Journal
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME
Volume 126, Issue 1, Pages 155-159Publisher
ASME-AMER SOC MECHANICAL ENG
DOI: 10.1115/1.1622409
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This paper summarizes recent enhancements to a probabilistic damage tolerance software code, DARWIN(TM),that can be used or design certification of aircraft jet engine titanium disks/rotors that may contain melt-related anomalies. Evaluations of DARWIN(TM) by engine manufacturers are also discussed, including comparisons with existing codes for accuracy and time efficiency In addition, relevant test results, including various fatigue tests on material containing melt-related anomalies, are summarized.
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