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Analysis, prediction, and prevention of edge delamination in rotor system structuresAnalytical methods such as simple sublaminate analysis, as well as quasi three-dimensional finite element analysis, provide insight into delamination characteristics and reliable trend data with which to make rapid evaluations of competitive concepts in the design environment. It is concluded that free edge delamination can be managed by analysis and prevented by design. However, in order to ensure durable composite structures, more work is needed to characterize delamination that occurs from other sources, such as matrix cracking and ply drops.
Document ID
19880035542
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chan, Wen S.
(Bell Helicopter Textron, Inc. Fort Worth, TX, United States)
Rehfield, Larry W.
(Georgia Institute of Technology Atlanta, United States)
O'Brien, T. Kevin
(NASA Langley Research Center; U.S. Army, Aerostructures Directorate, Hampton VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Composite Materials
Meeting Information
Meeting: AHS, Annual Forum
Location: Saint Louis, MO
Country: United States
Start Date: May 18, 1987
End Date: May 20, 1987
Accession Number
88A22769
Distribution Limits
Public
Copyright
Other

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