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Buckling of shells of revolution with various wall constructions. Volume 2 - Basic equations and method of solutionBasic equations and method of solution for computerized analysis of shells of revolution with axisymmetric collapse and nonsymmetric bifurcation buckling behavior
Document ID
19680013982
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Almroth, B. O. (Lockheed Aircraft Corp. Sunnyvale, CA, United States)
Bushnell, D. (Lockheed Aircraft Corp. Sunnyvale, CA, United States)
Sobel, L. H. (Lockheed Aircraft Corp. Sunnyvale, CA, United States)
Date Acquired
August 4, 2013
Publication Date
May 1, 1968
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-1050
LAC-4-17-67-1, V. 2
Report Number: NASA-CR-1050
Report Number: LAC-4-17-67-1, V. 2
Accession Number
68N23451
Funding Number(s)
CONTRACT_GRANT: NAS1-6073
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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