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Stress and stability investigations on thin-wall conical shells for axially symmetric boundary conditionsStress and stability of thin-walled conical shells for axisymmetric loads
Document ID
19670016998
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Schiffner, K. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
January 6, 1967
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-59676
RSIC-630
Report Number: NASA-TM-X-59676
Report Number: RSIC-630
Accession Number
67N26327
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STRUCTURAL STABILITY
THIN WALLED SHELL
CONICAL SHELL
SHELL THEORY
BUCKLING

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