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Test/semi-empirical analysis of a carbon/epoxy fabric stiffened panelThe purpose of this work-in-progress is to present a semi-empirical analysis method developed to predict the buckling and crippling loads of carbon/epoxy fabric blade stiffened panels in compression. This is a hand analysis method comprised of well known, accepted techniques, logical engineering judgements, and experimental data that results in conservative solutions. In order to verify this method, a stiffened panel was fabricated and tested. Both the best and analysis results are presented.
Document ID
19910000989
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Spier, E. E.
(Rohr Industries, Inc. San Diego, CA, United States)
Anderson, J. A.
(Rohr Industries, Inc. San Diego, CA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Publication Information
Publication: NASA, Langley Research Center, Research in Structures, Structural Dynamics, and Materials, 1990
Subject Category
Structural Mechanics
Accession Number
91N10302
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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