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NACA-TN-752: An investigation of sheet-stiffener panels subjected to compression loads with particular reference to torsionally weak stiffeners
Abstract: A total of 183 panel specimens of 24ST aluminum alloy with nominal thickness of 0.020, and 0.040 inch with extruded bulb-angle sections of 12 shapes spaced 4 and 5 inches as stiffeners were tested to obtain the buckling ...