This is the second of a series of reports covering an investigation of the general instability problem by the California Institute of Technology. The first five reports of this series cover investigations of the general instability problem under the loading conditions of pure bending and were prepared under the sponsorship of the Civil Aeronautics Administration. The succeeding reports of this series cover the work done on other loading conditions under the sponsorship of the National Advisory Committee for Aeronautics
Thirty-four circular cylinders stiffened by heavy rings were loaded to failure in combined bending a...
Compression tests on integrally stiffened cylinders - determination of loads and stresses associated...
Bending tests were made on a cylindrical semimonocoque shell of circular cross section. The cylinder...
This report summarizes the work that has been carried on in the experimental investigation of the pr...
This is the third of a series of reports covering an investigation of the general instability proble...
Results are presented of an experimental investigation of the general instability of reinforced thin...
This is the fourth of a series of reports covering an investigation of the general instability probl...
An experimental investigation of the general instability of reinforced thin-walled metal cylinders w...
This report summarizes the work that has been carried on in the experimental investigation of the pr...
Results are presented of an experimental investigation of the general instability of reinforced thin...
This is the sixth of a series of reports covering an investigation of the general instability proble...
Buckling data review for stiffened cylinder failures during axial compression and bendin
Results are presented of an experimental investigation of the general instability of reinforced thin...
Twenty-five ring-stiffened circular cylinders were loaded to failure in bending. The results are pre...
Eighteen 24S-T alclad cylinders of 20-inch diameter, with skin thickness varying between 0.012 inch ...
Thirty-four circular cylinders stiffened by heavy rings were loaded to failure in combined bending a...
Compression tests on integrally stiffened cylinders - determination of loads and stresses associated...
Bending tests were made on a cylindrical semimonocoque shell of circular cross section. The cylinder...
This report summarizes the work that has been carried on in the experimental investigation of the pr...
This is the third of a series of reports covering an investigation of the general instability proble...
Results are presented of an experimental investigation of the general instability of reinforced thin...
This is the fourth of a series of reports covering an investigation of the general instability probl...
An experimental investigation of the general instability of reinforced thin-walled metal cylinders w...
This report summarizes the work that has been carried on in the experimental investigation of the pr...
Results are presented of an experimental investigation of the general instability of reinforced thin...
This is the sixth of a series of reports covering an investigation of the general instability proble...
Buckling data review for stiffened cylinder failures during axial compression and bendin
Results are presented of an experimental investigation of the general instability of reinforced thin...
Twenty-five ring-stiffened circular cylinders were loaded to failure in bending. The results are pre...
Eighteen 24S-T alclad cylinders of 20-inch diameter, with skin thickness varying between 0.012 inch ...
Thirty-four circular cylinders stiffened by heavy rings were loaded to failure in combined bending a...
Compression tests on integrally stiffened cylinders - determination of loads and stresses associated...
Bending tests were made on a cylindrical semimonocoque shell of circular cross section. The cylinder...