Add to ORKGThe analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings
Equations are given for the elastic behavior of initially curved sheets in which the deflections are...
A total of 183 panel specimens of 24ST aluminum alloy with nominal thickness of 0.020, and 0.040 inc...
The results of a series of tests to determine the effect of internal pressure on the buckling load o...
The present experiments treat the stress of actual tension fields within the elastic range. They giv...
The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wri...
This note is on an investigation made to obtain information on the strength of thin curved sheets of...
This report continues the work presented in NACA-TM 605 and expands the scope to include the change ...
The object of the present experiments is a more exact determination of the effective width for the c...
This report describes experiments made for the purpose of ascertaining the effective width of circul...
The design of curved sheet panels to resist shear involves a consideration of several factors: the b...
This report presents the results of an investigation to determine the behavior of dural strip with f...
A total of 183 panel specimens of 24ST aluminum alloy with nominal thickness of 0.020, 0.025, and 0....
A total of 183 panel specimens of 24ST aluminum alloy with nominal thickness of 0.020, 0.025, and 0....
The object of this report was to develop the structural method of sheet metal girders and should for...
This report covers a series of tests on thin flat elastic strips restrained at two parallel edges an...
Equations are given for the elastic behavior of initially curved sheets in which the deflections are...
A total of 183 panel specimens of 24ST aluminum alloy with nominal thickness of 0.020, and 0.040 inc...
The results of a series of tests to determine the effect of internal pressure on the buckling load o...
The present experiments treat the stress of actual tension fields within the elastic range. They giv...
The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wri...
This note is on an investigation made to obtain information on the strength of thin curved sheets of...
This report continues the work presented in NACA-TM 605 and expands the scope to include the change ...
The object of the present experiments is a more exact determination of the effective width for the c...
This report describes experiments made for the purpose of ascertaining the effective width of circul...
The design of curved sheet panels to resist shear involves a consideration of several factors: the b...
This report presents the results of an investigation to determine the behavior of dural strip with f...
A total of 183 panel specimens of 24ST aluminum alloy with nominal thickness of 0.020, 0.025, and 0....
A total of 183 panel specimens of 24ST aluminum alloy with nominal thickness of 0.020, 0.025, and 0....
The object of this report was to develop the structural method of sheet metal girders and should for...
This report covers a series of tests on thin flat elastic strips restrained at two parallel edges an...
Equations are given for the elastic behavior of initially curved sheets in which the deflections are...
A total of 183 panel specimens of 24ST aluminum alloy with nominal thickness of 0.020, and 0.040 inc...
The results of a series of tests to determine the effect of internal pressure on the buckling load o...