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Transient analysis using conical shell elementsThe use of the NASTRAN conical shell element in static, eigenvalue, and direct transient analyses is demonstrated. The results of a NASTRAN static solution of an externally pressurized ring-stiffened cylinder agree well with a theoretical discontinuity analysis. Good agreement is also obtained between the NASTRAN direct transient response of a uniform cylinder to a dynamic end load and one-dimensional solutions obtained using a method of characteristics stress wave code and a standing wave solution. Finally, a NASTRAN eigenvalue analysis is performed on a hydroballistic model idealized with conical shell elements.
Document ID
19740006482
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yang, J. C. S.
(Naval Ordnance Lab. Silver Spring, MD, United States)
Goeller, J. E.
(Naval Ordnance Lab. Silver Spring, MD, United States)
Messick, W. T.
(Naval Ordnance Lab. Silver Spring, MD, United States)
Date Acquired
August 7, 2013
Publication Date
September 1, 1973
Publication Information
Publication: NASA. Langley Res. Center NASTRAN: Users' Experiences
Subject Category
Structural Mechanics
Accession Number
74N14595
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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