Response to comments on ‘effect of prior processing on the performance of PH 13-8 Mo stainless steel helicopter components’
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The conclusions drawn for this investigation seemed appropriate from the results obtained. It is true that machining may have played a role in the components tested at AATD, but ARL does not feel this was the root cause of the premature “C” rod failures.
KeywordsFatigue Material Specimen Practical Failure Analysis Volume Tool Mark Thread Root
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