Critical Compressive Stress for Outstanding Flanges Page: 4 of 11
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REPORT NO. 734--NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS
FrIGuz 2.- Concluded.
111 N I 1 2I'I2 Ih 11 1- 1m
U 20 24 28 32 3 40 4 4 48 0 20 24 28 32 36 40 44 48
, kios/sq in. f, kA s/sq h7.i
F on 4.--Varlation of , a , , and w ith the ompressive stress f for 248-T Fzraoua .--Variation of r , r ,h and withhecompressive stresf for 248-T lumi-
aluminum alloy of minimum required properties. num alloy of average properties.
T + 3T
S; 7 _ i i
LI [ .I.T +
~~ .9 .A_ .'0%.P
i-" r 3 Y
i i rI i
~ 91 IL
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Lundquist, Eugene E. & Stowell, Elbridge Z. Critical Compressive Stress for Outstanding Flanges, report, March 14, 1941; (digital.library.unt.edu/ark:/67531/metadc59989/m1/4/: accessed January 16, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.