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Accession Number:
AD0842809
Title:
Study of Fatigue Crack Initiation from Flaws Using Fracture Mechanics Theory
Descriptive Note:
Rept. for Jul 1966-Aug 1967
Corporate Author:
AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH
Report Date:
1968-09-01
Pagination or Media Count:
33.0
Distribution Statement:
APPROVED FOR PUBLIC RELEASE