Bending tests were made of two circular cylinders of corrugated aluminum-alloy sheet. In each test failure occurred by bending of the corrugations in a plane normal to the skin. It was found, after analysis of the effect of short end bays, that the computed stress on the extreme fiber of a corrugated cylinder is in excess of that for a flat panel of the same basic pattern and panel length tested as a pin-ended column. It is concluded that this increased strength was due to the effects of curvature of the pitch line. It is also concluded from the tests that light bulkheads closely spaced strengthen corrugated cylinders very materially
This report is the first of a series presenting the results of strength tests on thin-walled cylinde...
Tests were made to determine the effect of brake forming on the strength of 24S-T aluminum alloy she...
Static tests on paper cylinders were conducted at the Langley Memorial Aeronautical Laboratory at La...
Bending tests were made of two circular cylinders of corrugated aluminum-alloy sheet. In each test f...
This report is the third of a series presenting the results of strengths tests on thin-walled cylind...
Bending tests were made on a cylindrical semimonocoque shell of circular cross section. The cylinder...
This report is the fourth of a series presenting the results of strength tests on thin-walled cylind...
This report describes experiments made for the purpose of ascertaining the effective width of circul...
A monocoque box beam consisting of a 24S-T aluminum-alloy sheet reinforced by four bulkheads and by ...
This note is on an investigation made to obtain information on the strength of thin curved sheets of...
Ten 24S-T alclad cylinders of 20-inch diameter, 45- or 58-inch length, and 0.012-inch wall thickness...
Eighteen 24S-T alclad cylinders of 20-inch diameter, with skin thickness varying between 0.012 inch ...
Results are presented for a part of a test program on 24S-T aluminum alloy flat compression panels w...
This report gives a comparison of the accuracy of the three methods for calculating the compressive ...
Experiments were carried out at Polytechnic Institute of Brooklyn Aeronautical Laboratories in order...
This report is the first of a series presenting the results of strength tests on thin-walled cylinde...
Tests were made to determine the effect of brake forming on the strength of 24S-T aluminum alloy she...
Static tests on paper cylinders were conducted at the Langley Memorial Aeronautical Laboratory at La...
Bending tests were made of two circular cylinders of corrugated aluminum-alloy sheet. In each test f...
This report is the third of a series presenting the results of strengths tests on thin-walled cylind...
Bending tests were made on a cylindrical semimonocoque shell of circular cross section. The cylinder...
This report is the fourth of a series presenting the results of strength tests on thin-walled cylind...
This report describes experiments made for the purpose of ascertaining the effective width of circul...
A monocoque box beam consisting of a 24S-T aluminum-alloy sheet reinforced by four bulkheads and by ...
This note is on an investigation made to obtain information on the strength of thin curved sheets of...
Ten 24S-T alclad cylinders of 20-inch diameter, 45- or 58-inch length, and 0.012-inch wall thickness...
Eighteen 24S-T alclad cylinders of 20-inch diameter, with skin thickness varying between 0.012 inch ...
Results are presented for a part of a test program on 24S-T aluminum alloy flat compression panels w...
This report gives a comparison of the accuracy of the three methods for calculating the compressive ...
Experiments were carried out at Polytechnic Institute of Brooklyn Aeronautical Laboratories in order...
This report is the first of a series presenting the results of strength tests on thin-walled cylinde...
Tests were made to determine the effect of brake forming on the strength of 24S-T aluminum alloy she...
Static tests on paper cylinders were conducted at the Langley Memorial Aeronautical Laboratory at La...