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On the elastic stability of shellsA synopsis of a series of investigations into the instability of axially compressed cylindrical shells is given. The objective of the research, which was made with models, was to devise a technique of nondestructive evaluation. The results show that, with models at any rate, success was achieved. Probing methods which can be used to determine the locations of weakness and the pertinent instability load levels were devised. The research on large scale shells was undertaken to determine the critical loads under as uniform a circumferential distribution of axial compressive force as possible. It is clear from the results presented that this objective was met.
Document ID
19760024480
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Horton, W. H.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1976
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-148484
Report Number: NASA-CR-148484
Accession Number
76N31568
Funding Number(s)
CONTRACT_GRANT: NGL-11-002-096
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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