Search
Now showing items 1-10 of 16
NACA-TN-1851: Critical shear stress of infinitely long, simply supported plate with transverse stiffeners
Abstract: A theoretical solution is given for the critical shear stress of an infinitely long, simply supported, flat plate with identical, equally spaced, transverse stiffeners of zero tensional stiffness. Results are obtained by ...
NACA-TR-733: Critical Compressive Stress for Flat Rectangular Plates Supported Along All Edges and Elastically Restrained Against Rotation along the Unloaded Edges
Abstract: A 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 flat rectangular plates supported along all edges and, in addition, ...
NACA-TN-3784: Handbook of structural stability part IV - failure of plates and composite elements
Abstract: Available theories on failure of flat plates are reviewed, and test data on the postbuckling behavior, effective width, and failure of flat curved plates are correlated. Test data on the crippling strength of various formed ...
NACA-TN-427: Strength tests on thin-walled duralumin cylinders in torsion
Abstract: This report is the first of a series presenting the results of strength tests on thin-walled cylinders and truncated cones of circular and elliptical section; it comprises the results obtained to date from torsion (pure ...
NACA-TR-734: Critical Compressive Stress for Outstanding Flanges
Abstract: A 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 ...
NACA-TR-827: Charts for the minimum-weight design of 24s-t aluminum-alloy flat compression panels with longitudinal z-section stiffeners
Abstract: Design charts are developed for 24s-t aluminum-alloy flat compression panels with longitudinal z-section stiffeners. These charts make possible the design of the lightest panels of this type for a wide range of design ...
NACA-TR-1027: Buckling of thin-walled cylinder under axial compression and internal pressure
Abstract: An investigation was made of a thin-walled cyclinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predicted increase of compressive buckling stress due ...
NACA-ARR-4B03: Compressive strength of flat panels with Z-section stiffeners
Abstract: INTRODUCTION
Several series of compression tests have been made on panels with Z-section stiffeners formed from flat sheet (see fig.1) to show the importance of relative dimensions in determining the strength of ...
Several series of compression tests have been made on panels with Z-section stiffeners formed from flat sheet (see fig.1) to show the importance of relative dimensions in determining the strength of ...
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 ...
NACA-TN-1553: Compressive strength of 24S-T aluminum-alloy flat panels with longitudinal formed hat-section stiffeners having four ratios of stiffener thickness to skin thickness
Abstract: Results are presented for a test program on 24S-T aluminum-alloy flat compression panels with longitudinal formed hat-section stiffeners. The results for panels in which the thickness are presented and incorporated with ...