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Design detail verification tests for a lightly loaded open-corrugation graphite-epoxy cylinderFlat corrugated graphite-epoxy panels were tested in compression to verify selected design details of a ring-stiffened cylinder that was designed to support an axial compressive load of 157.6 kN/m without buckling. Three different sizes of subcomponent panels, with the same basic corrugation geometry, were tested: (1) 60.96-cm-long by 45.72-cm-wide panels to evaluate the local buckling strength of the shell wall design; (2) 91.44-cm-long by 45.72-cm-wide panels to evaluate a longitudinal joint and the load-introduction method; and (3) 254.0-cm-long by 91.44-cm-wide panels with four simulated-ring stiffeners to evaluate the ring-attachment method. The test results indicate that the modified shell-wall design, the longitudinal joint, the load-introduction method, and the stiffener-attachment method for the proposed cylinder have adequate strength to support the design load.
Document ID
19820012693
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Davis, R. C.
(NASA Langley Research Center Hampton, VA, United States)
Starnes, J. H., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1982
Subject Category
Structural Mechanics
Report/Patent Number
L-14795
NAS 1.60:1981
NASA-TP-1981
Report Number: L-14795
Report Number: NAS 1.60:1981
Report Number: NASA-TP-1981
Accession Number
82N20567
Funding Number(s)
PROJECT: RTOP 506-53-43-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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