A fixture is described for making normal-pressure tests of flat plates 5 inches in diameter in which particular care was taken to obtain rigid clamping at the edges. Results are given for 19 plates, ranging in thickness from 0.015 to 0.072 inch. The center deflections and the extreme-fiber stresses at low pressures were found to agree with theoretical values; the center deflections at high pressures were 4 to 12 percent greater than the theoretical values. Empirical curves are derived of the pressure for the beginning of permanent set as a function of the dimensions of the plate and the tensile properties of the material
Available theories on failure of flat plates are reviewed, and test data on the postbuckling behavio...
This report gives a comparison of the accuracy of the three methods for calculating the compressive ...
Available theories and test data on buckling of curved plates and shells are reviewed. For torsion a...
A fixture is described for making normal-pressure tests of flat plates 5 inches in diameter in which...
A theoretical analysis is given for the stresses and deflections of a square plate with clamped edge...
The von Karman equations for flat plates are solved beyond the buckling load up to edge strains equa...
Flat rectangular plates of duralumin, stainless iron, monel metal, and nickel were tested under load...
Flat sheet panels of aluminum alloy (all 17S-T except for two specimens of 24S-T) were tested under ...
The Von Karman equations for a thin flat plate with large deflections are solved for the special cas...
Results are presented for a part of a test program on 24S-T aluminum alloy flat compression panels w...
The various factors governing buckling of flat plates are critically reviewed and the results are su...
The results of a theoretical and experimental investigation to determine the critical compression lo...
An aluminum-alloy plate containing an open circular hole of diameter large compared with the thickne...
An analysis is presented of the postbuckling behavior of a simply supported square flat plate with s...
The present experiments treat the stress of actual tension fields within the elastic range. They giv...
Available theories on failure of flat plates are reviewed, and test data on the postbuckling behavio...
This report gives a comparison of the accuracy of the three methods for calculating the compressive ...
Available theories and test data on buckling of curved plates and shells are reviewed. For torsion a...
A fixture is described for making normal-pressure tests of flat plates 5 inches in diameter in which...
A theoretical analysis is given for the stresses and deflections of a square plate with clamped edge...
The von Karman equations for flat plates are solved beyond the buckling load up to edge strains equa...
Flat rectangular plates of duralumin, stainless iron, monel metal, and nickel were tested under load...
Flat sheet panels of aluminum alloy (all 17S-T except for two specimens of 24S-T) were tested under ...
The Von Karman equations for a thin flat plate with large deflections are solved for the special cas...
Results are presented for a part of a test program on 24S-T aluminum alloy flat compression panels w...
The various factors governing buckling of flat plates are critically reviewed and the results are su...
The results of a theoretical and experimental investigation to determine the critical compression lo...
An aluminum-alloy plate containing an open circular hole of diameter large compared with the thickne...
An analysis is presented of the postbuckling behavior of a simply supported square flat plate with s...
The present experiments treat the stress of actual tension fields within the elastic range. They giv...
Available theories on failure of flat plates are reviewed, and test data on the postbuckling behavio...
This report gives a comparison of the accuracy of the three methods for calculating the compressive ...
Available theories and test data on buckling of curved plates and shells are reviewed. For torsion a...