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Methods and formulas for calculating the strength of plate and shell constructions as used in airplane designThis report is a compilation of previously published articles on formulas and methods of calculation for the determination of the strength and stability of plate and shell construction as employed in airplane design. In particular, it treats the problem of isotropic, orthotopic, and stiffened rectangular plates, thin curved panels, and circular cylinders under various loading conditions. The purpose of appending the pertinent literature references following the subjects discussed was to facilitate a comprehensive study of the treated problems.
Document ID
19930094632
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Heck, O S
Ebner, H
Date Acquired
September 6, 2013
Publication Date
February 1, 1936
Report/Patent Number
NACA-TM-785
Accession Number
93R23552
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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