Stress is derived for simply supported panel in axial compression having stiffener offering no torsional restraint; results presented in form of curves and table; because panel of moderate or large curvature buckles in compression at stress considerably below theoretical value, method is suggested to aid in determining critical stress for use in design.
Critical axial-compressive stress of curved rectangular panel with Central chordwise stiffener
Nat Advisory Committee Aeronautics -- Tech Note
1948
23 pages
Report
English
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Critical axial-compressive stress of curved rectangular panel with Central longitudinal stiffener
Engineering Index Backfile | 1949
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