Part of test program given is concerned with panels in which thickness of stiffener material is 0.625 times skin thickness; results show effect of relative dimensions of panel on buckling stress; comparative envelope curves for hat stiffened and Z-stiffened panels provide indication of relative structural efficiencies of two types of panel.
Compressive strength of 24S-T aluminum-alloy flat panels with longitudinal formed hat-section stiffeners
Nat Advisory Committee Aeronautics -- Tech Note
1946
10 pages
12 Supp plates
Article (Journal)
English
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Engineering Index Backfile | 1949
|Compressive strength of flat panels with Z-section stiffeners
TIBKAT | 1944
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