NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Juncture stress fields in multicellular shell structures. Volume VIII - Buckling analysis of segmental orthotropic cylinders under non-uniform stress distribution Final technical reportOrthotropic cylindrical shell buckling under axial compression - structural dynamics
Document ID
19660006962
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Almroth, B. O. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Brogan, F. A. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Pittner, E. V. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 3, 2013
Publication Date
December 1, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-69995
M-77-65-8
Report Number: NASA-CR-69995
Report Number: M-77-65-8
Accession Number
66N16251
Funding Number(s)
CONTRACT_GRANT: NAS8-11480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STRUCTURAL DYNAMICS
ORTHOTROPIC CYLINDER
COMPRESSION BUCKLING
AXIAL COMPRESSION
CYLINDRICAL SHELL

Related Records

There are no records associated with this record.
No Preview Available