In order to determine the critical stresses caused by an outward acting pressure on the upper surface of a wing due to the difference in internal and external pressures, torsional tests were made on two curved-sheet specimens subjected to an outward acting normal pressure. Results show that an outward acting normal pressure appreciable raises the critical shear stress for an unstiffened curved sheet; the absolute increase in critical shear stress is slightly greater for a 30 in. rib spacing than for a 10 in. rib spacing
In practice the actual maximum stress is greater than the stress determined by the simple girder the...
This note presents the results of flight pressure-distribution tests on the right upper wing panel o...
The design of curved sheet panels to resist shear involves a consideration of several factors: the b...
Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of n...
Results are presented of tests of two specimens tested to study the effect of normal pressure on the...
In order to determine the critical stresses caused by an outward acting pressure on the upper surfac...
The results of a series of tests to determine the effect of internal pressure on the buckling load o...
Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of n...
This report presents the results of an investigation to determine the behavior of dural strip with f...
The design of curved sheet panels to resist shear involves a consideration of several factors: the b...
This note is on an investigation made to obtain information on the strength of thin curved sheets of...
Tests were made on 18 shear panels of 24S-T aluminum alloy to verify the dependence of the ultimate ...
Panels of aluminum alloy sheets, framed by side and end stiffeners, were subjected to combined loadi...
The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wri...
This investigation was undertaken to study the distribution of loading over thick wings of various t...
In practice the actual maximum stress is greater than the stress determined by the simple girder the...
This note presents the results of flight pressure-distribution tests on the right upper wing panel o...
The design of curved sheet panels to resist shear involves a consideration of several factors: the b...
Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of n...
Results are presented of tests of two specimens tested to study the effect of normal pressure on the...
In order to determine the critical stresses caused by an outward acting pressure on the upper surfac...
The results of a series of tests to determine the effect of internal pressure on the buckling load o...
Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of n...
This report presents the results of an investigation to determine the behavior of dural strip with f...
The design of curved sheet panels to resist shear involves a consideration of several factors: the b...
This note is on an investigation made to obtain information on the strength of thin curved sheets of...
Tests were made on 18 shear panels of 24S-T aluminum alloy to verify the dependence of the ultimate ...
Panels of aluminum alloy sheets, framed by side and end stiffeners, were subjected to combined loadi...
The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wri...
This investigation was undertaken to study the distribution of loading over thick wings of various t...
In practice the actual maximum stress is greater than the stress determined by the simple girder the...
This note presents the results of flight pressure-distribution tests on the right upper wing panel o...
The design of curved sheet panels to resist shear involves a consideration of several factors: the b...