Author: Marvin B. Dow
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 32
Book Description
Bending and Compression Tests of Pressurized Ring-stiffened Cylinders
Author: Marvin B. Dow
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 32
Book Description
Structural Behavior of Pressurized, Ring-stiffened, Thin-wall Cylinders Subjected to Axial Compression
General Instability of Orthotropically Stiffened Cylinders
Author: C. Lakshmikantham
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 58
Book Description
As part of a general program to determine the applicability of linear orthotropic theory to the design of cylindrical shells under various loading conditions, a theoretical and experimental investigation was performed on the general instability of orthotropic cylinders under bending and combined axial compression and bending loading. Based on a simple approximation for the asymmetric buckling pattern, theoretical results suitable for design use were obtained for the buckling of orthotropic cylinders for both bending and combined loading conditions. It was shown that the buckling stress for orthotropic cylinders under bending or axial compression loading are equal which agrees with previous results for isotropic cylinders. Theoretical results were evaluated by means of a series of careful experiments performed on orthotropically stiffened cylinders designed to fail in the elastic general instability mode. For both bending loading and the combined axial and bending loading condition, experimental results were in good agreement with the theory.
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 58
Book Description
As part of a general program to determine the applicability of linear orthotropic theory to the design of cylindrical shells under various loading conditions, a theoretical and experimental investigation was performed on the general instability of orthotropic cylinders under bending and combined axial compression and bending loading. Based on a simple approximation for the asymmetric buckling pattern, theoretical results suitable for design use were obtained for the buckling of orthotropic cylinders for both bending and combined loading conditions. It was shown that the buckling stress for orthotropic cylinders under bending or axial compression loading are equal which agrees with previous results for isotropic cylinders. Theoretical results were evaluated by means of a series of careful experiments performed on orthotropically stiffened cylinders designed to fail in the elastic general instability mode. For both bending loading and the combined axial and bending loading condition, experimental results were in good agreement with the theory.
Correlation of the Buckling Strength of Pressurized Cylinders in Compression Or Bending with Structural Parameters
Author: James P. Peterson
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Buckling (Mechanics)
Languages : en
Pages : 28
Book Description
NASA Technical Note
The General Instability of Ring-stiffened Corrugated Cylinders Under Axial Compression
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.
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.
Bending Tests of Large-diameter Ring-stiffened Corrugated Cylinders
Author: James P. Peterson
Publisher:
ISBN:
Category : Bending fatigue
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Bending fatigue
Languages : en
Pages : 44
Book Description
Correlation of the Buckling Strength of Pressurized Cylinders in Compression Or Bending with Structural Parameters
Author: James P. Peterson
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
The data on nonpressurized cylinders in bending of NACA TN 3735 and the data on pressurized cylinders in compression and bending of NASA TN D-360 are correlated with structural parameters by using small-deflection buckling theory and reduced values for the extensional stiffness of the cylinder wall. The correlating procedure should prove useful in future shell-buckling investigations by reducing the number of tests required.
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
The data on nonpressurized cylinders in bending of NACA TN 3735 and the data on pressurized cylinders in compression and bending of NASA TN D-360 are correlated with structural parameters by using small-deflection buckling theory and reduced values for the extensional stiffness of the cylinder wall. The correlating procedure should prove useful in future shell-buckling investigations by reducing the number of tests required.
Bending Tests of Large-diameter Stiffened Cylinders Susceptible to General Instability
Author: Michael F. Card
Publisher:
ISBN:
Category : Bending
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Bending
Languages : en
Pages : 44
Book Description
Buckling Experiments: Experimental Methods in Buckling of Thin-Walled Structures, Volume 2
Author: Josef Singer
Publisher: John Wiley & Sons
ISBN: 0471974501
Category : Technology & Engineering
Languages : en
Pages : 1140
Book Description
* Edited by Josef Singer, the world's foremost authority on structural buckling. * Time-saving and cost-effective design data for all structural, mechanical, and aerospace engineering researchers.
Publisher: John Wiley & Sons
ISBN: 0471974501
Category : Technology & Engineering
Languages : en
Pages : 1140
Book Description
* Edited by Josef Singer, the world's foremost authority on structural buckling. * Time-saving and cost-effective design data for all structural, mechanical, and aerospace engineering researchers.