Author: F. G. Morton
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
Book Description
The report contains results of an experimental investigation to determine the stresses in a thin-walled cylindrical shell subjected to a radial load applied by a small, rectangular pad. Four loading devices are studies: 3 rubberlined pad configurations, 1 pneumatic bag, constrained to apply a load over a rectangular area. There is sufficient duplication of test parameters to check repeatability of results. The test results show rather close agreement with available theoretical values. (Author).
Stress and Stability Analysis of Cylindrical and Conical Shells. Volume Iii. an Experimental Investigation of the Stress in Cylindrical Shells Subjected to Small Pad Loads
Author: F. G. Morton
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
Book Description
The report contains results of an experimental investigation to determine the stresses in a thin-walled cylindrical shell subjected to a radial load applied by a small, rectangular pad. Four loading devices are studies: 3 rubberlined pad configurations, 1 pneumatic bag, constrained to apply a load over a rectangular area. There is sufficient duplication of test parameters to check repeatability of results. The test results show rather close agreement with available theoretical values. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
Book Description
The report contains results of an experimental investigation to determine the stresses in a thin-walled cylindrical shell subjected to a radial load applied by a small, rectangular pad. Four loading devices are studies: 3 rubberlined pad configurations, 1 pneumatic bag, constrained to apply a load over a rectangular area. There is sufficient duplication of test parameters to check repeatability of results. The test results show rather close agreement with available theoretical values. (Author).
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 780
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 780
Book Description
Government-wide Index to Federal Research & Development Reports
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 840
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 840
Book Description
U.S. Government Research & Development Reports
Author:
Publisher:
ISBN:
Category : Technology
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category : Technology
Languages : en
Pages :
Book Description
U.S. Government Research and Development Reports
Author:
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1352
Book Description
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1352
Book Description
Government Reports Announcements
Author:
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1300
Book Description
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 1300
Book Description
Bibliography of Scientific and Industrial Reports
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1366
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1366
Book Description
Government Reports Annual Index
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 834
Book Description
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 834
Book Description
Stress and Stability Analysis of Cylindrical and Conical Shells. Volume Iv. Response of Thin-walled Cylindrical Shells to Saddletype Loads
Author: D. O. Brush
Publisher:
ISBN:
Category :
Languages : en
Pages : 74
Book Description
Results are presented of an experimental investigation of unstiffened, thin-walled cylindrical shells subjected to a transverse load applied by a cushioned saddle. The cylinders were supported at the ends and the saddle load applied at midspan. Prebuckling stresses, buckling mode, and buckling load were investigated. All of the test cylinders failed in a mode that is characteristic of unstiffened cylindrical shell failure under local circumferential stresses. The only independent variable investigated in the test series was the stiffness of the saddle liner material. The liner stiffness was found to have a strong influence on the magnitude of the buckling load, with stiffer liners resulting in higher buckling loads. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 74
Book Description
Results are presented of an experimental investigation of unstiffened, thin-walled cylindrical shells subjected to a transverse load applied by a cushioned saddle. The cylinders were supported at the ends and the saddle load applied at midspan. Prebuckling stresses, buckling mode, and buckling load were investigated. All of the test cylinders failed in a mode that is characteristic of unstiffened cylindrical shell failure under local circumferential stresses. The only independent variable investigated in the test series was the stiffness of the saddle liner material. The liner stiffness was found to have a strong influence on the magnitude of the buckling load, with stiffer liners resulting in higher buckling loads. (Author).
Stress and Stability Analysis of Cylindrical and Conical Shells. Volume I. an Infinitesimal-buckling Analysis for Truncated Conical Shells Subjected to External Pressure
Author: E. V. Pittner
Publisher:
ISBN:
Category :
Languages : en
Pages : 47
Book Description
An approximate energy analysis for determining the buckling load of a thin truncated conical shell under combined axial compression and external lateral pressure is presented. Numerical examples based on the present theory are given for cones subjected to hydrostatic pressure. Calculated buckling pressures for this loading are compared with results of other analyses and of recent tests. Results of the present analysis are in close agreement with these tests and with certain of the other analyses. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 47
Book Description
An approximate energy analysis for determining the buckling load of a thin truncated conical shell under combined axial compression and external lateral pressure is presented. Numerical examples based on the present theory are given for cones subjected to hydrostatic pressure. Calculated buckling pressures for this loading are compared with results of other analyses and of recent tests. Results of the present analysis are in close agreement with these tests and with certain of the other analyses. (Author).