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Critical Compressive Stress for Outstanding FlangesA 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 outstanding flanges. These flanges are flat rectangular plates supported along the loaded edges, supported and elastically restrained along one unloaded edge, and free along the other unloaded edge. The mathematical derivations of the formulas required for construction of the chart are given.
Document ID
19930091812
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Report
Authors
Lundquist, Eugene E
Stowell, Elbridge Z
Date Acquired
September 6, 2013
Publication Date
January 1, 1942
Report/Patent Number
NACA-TR-734
Report Number: NACA-TR-734
Accession Number
93R21102
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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