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Critical Compressive Stress for Flat Rectangular Plates Supported Along all Edges and Elastically Restrained Against Rotation Along the Unloaded Edges, Special Report 189A chart is presented for the values of the coefficient in the formula for the critical compressive stress at which buckling may be expected to occur in flat rectangular plates supported along all edges and, in addition, elastically restrained against rotation along the unloaded edges. The mathematical derivations of the formulas required in the construction of the chart are given.
Document ID
20090015033
Document Type
Other
Authors
Lundquist, Eugene E.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Stowell, Eldbridge Z.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 1941
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-SR-189
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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