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Fatigue crack propagation in stiffened panelsFatigue crack propagation in Al alloy panels stiffened with bolted and integral stringers, determining stress intensity factor/crack growth rate relationship
Document ID
19710054459
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Poe, C. C., Jr.
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publisher: AMERICAN SOCIETY FOR TESTING AND MATERIALS,
Subject Category
Structural Mechanics
Meeting Information
Meeting: DAMAGE TOLERANCE IN AIRCRAFT STRUCTURES ANNUAL MEETING
Location: TORONTO
Country: CANADA
Start Date: June 21, 1970
End Date: June 26, 1970
Sponsors: AMERICAN SOCIETY FOR TESTING AND MATERIALS
Accession Number
71A35156
Distribution Limits
Public
Copyright
Other

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