Buckling of Thin-walled Cylinder Under Axial Compression and Internal Pressure PDF Download
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Author: Hsu Lo Publisher: ISBN: Category : Buckling (Mechanics) Languages : en Pages : 36
Book Description
An investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predicted increase of compressive buckling stress due to internal pressure agrees fairly well with the experimental results.
Author: Hsu Lo Publisher: ISBN: Category : Buckling (Mechanics) Languages : en Pages : 36
Book Description
An investigation was made of a thin-walled cylinder under axial compression and various internal pressures to study the effect of the internal pressure on the compressive buckling stress of the cylinder. A theoretical analysis based on a large-deflection theory was also made. The theoretically predicted increase of compressive buckling stress due to internal pressure agrees fairly well with the experimental results.
Author: LeRoy Earl Thompson Publisher: ISBN: Category : Buckling (Mechanics) Languages : en Pages : 80
Book Description
"An experimental investigation was made of the effects of internal pressure upon the buckling of thin circular cylindrical shells under axial compression. A comparison was made of the experimental and theoretical results; the latter were derived from the large-deflection theory. Results showed that the internal pressure had an appreciable strengthening effect upon the buckling of the cylindrical shell. The comparison showed that the experimental results were lower than the theoretical results for a given internal pressure. The discrepancy between the results can be expected since there were factors not included in the theory: imperfections, end conditions, lengths, and material irregularities"--Abstract, leaf ii.
Author: John N. Dickson Publisher: ISBN: Category : Axial flow compressors Languages : en Pages : 44
Book Description
A method is presented to determine the general instability load of a ring-stiffened corrugated cylinder under axial compression. This method is developed using linear small deflection theory. The stiffness properties of the rings are uniformly distributed along the cylinder and the eccentricity of the rings with respect to the corrugation centerline is taken into account. Analytical and experimental results are compared. In this comparison good agreement is obtained for cylinders loaded in pure compression. For the cylinders subjected to bending or a combination of bending and compression the analytical calculations are conservative. A computer program for the application of this method has been developed. The program and an explanation of its notation are included in this report.
Author: Hsu Lo
Author: Hsu Lo
Author: Hsu Lo
Author: Y. C. Fung
Author: Engineering Sciences Data Unit
Author: Don O. Brush
Author: James P. Peterson
Author: Marvin B. Dow
Author: Engineering Sciences Data Unit
Author: LeRoy Earl Thompson
Author: John N. Dickson