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Study of Size Effect in Sheet-stringer PanelsAn investigation was conducted to determine whether there are significant size effects in compressive strength of large Z-stiffened sheet-stringer panels as compared with geometrically similar smaller models and thus to ascertain whether the prediction of the strength of large panels by model tests is reliable. The specimens studied were manufactured from 7075-T6 aluminum alloy and included four representative types of panel designs, with full- and one-quarter-scale panels of each type.
Document ID
19930084675
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Doman, J P
(Naval Air Material Center)
Schwartz, Edward B
(Naval Air Material Center)
Date Acquired
August 16, 2013
Publication Date
July 1, 1956
Report/Patent Number
NACA-TN-3756
Report Number: NACA-TN-3756
Accession Number
93R13965
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOADS AND STRESSES, STRUCTURAL - COMPRESSION
PLATES, FLAT - STIFFENED
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