Fatigue crack growth from bolt holes of the 5th stage compressor discs of the J85-CAN-40 engines.

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TypeArticle
ConferenceICAS 2002 - 08-10 Sep 2002, Toronto
Subjectlife prediction; gas turbine engine; fracture mechanics
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionavailable
unclassified
unlimited
Peer reviewedYes
NRC numberSMPL-2001-0179
NPARC number8931378
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Record identifier010f15b0-0148-451e-ba7d-461d1c4fe47a
Record created2009-04-23
Record modified2016-05-09
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