Publication Date:
2013-08-31
Description:
The 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.
Keywords:
STRUCTURAL MECHANICS
Type:
NASA, Langley Research Center, Research in Structures, Structural Dynamics, and Materials, 1990; p 3-35
Format:
application/pdf
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