Masters Theses
Abstract
"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, page ii.
Advisor(s)
Senne, Joseph H.
Committee Member(s)
Joiner, James W., 1931-2013
Spooner, James Ernest
Schaefer, Rodney A., 1926-2002
Department(s)
Civil, Architectural and Environmental Engineering
Degree Name
M.S. in Civil Engineering
Publisher
University of Missouri at Rolla
Publication Date
1965
Pagination
viii, 40 pages
Rights
© 1965 LeRoy E. Thompson, All rights reserved.
Document Type
Thesis - Open Access
File Type
text
Language
English
Subject Headings
Buckling (Mechanics)Cylinders -- FatigueShells (Engineering)Thin-walled structures
Thesis Number
T 1732
Print OCLC #
5967158
Electronic OCLC #
802251381
Recommended Citation
Thompson, LeRoy E., "Effects of internal pressure upon the buckling of thin circular cylindrical shells under axial compression" (1965). Masters Theses. 5231.
https://scholarsmine.mst.edu/masters_theses/5231
