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Structural efficiencies of five compression panels with curved elementsStructural-efficiency analyses are used to determine the minimum-mass proportions of some panel configurations loaded in uniaxial compression. Five panel constructions, four of which incorporate circular-arc elements and the other a beaded-web corrugation, are shown to have improved structural efficiencies over conventional configurations. In addition to the structural-efficiency equations, which give the mass equivalent flat-plate thickness of the panel necessary to carry a given load, related design equations for calculating the cross-sectional dimensions of these minimum-mass panels are presented. The upper and lower limits of loading, where the design constraints of minimum gage or material yield strength become the dominant design conditions, are established and the corresponding design equations which are applicable outside these limits are also presented.
Document ID
19720005269
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Giles, G. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1971
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-6479
L-6546
Report Number: NASA-TN-D-6479
Report Number: L-6546
Accession Number
72N12918
Funding Number(s)
PROJECT: RTOP 134-14-05-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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