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Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling, and free vibration analysesAn improved four-node quadrilateral assumed-stress hybrid shell element with drilling degrees of freedom is presented. The formulation is based on Hellinger-Reissner variational principle and the shape functions are formulated directly for the four-node element. The element has 12 membrane degrees of freedom and 12 bending degrees of freedom. It has nine independent stress parameters to describe the membrane stress resultant field and 13 independent stress parameters to describe the moment and transverse shear stress resultant field. The formulation encompasses linear stress, linear buckling, and linear free vibration problems. The element is validated with standard tests cases and is shown to be robust. Numerical results are presented for linear stress, buckling, and free vibration analyses.
Document ID
19950006750
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rengarajan, Govind
(Clemson Univ. SC, United States)
Aminpour, Mohammad A.
(Clemson Univ. SC, United States)
Knight, Norman F., Jr.
(Clemson Univ. SC, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-192816
NAS 1.26:192816
Report Number: NASA-CR-192816
Report Number: NAS 1.26:192816
Accession Number
95N13163
Funding Number(s)
CONTRACT_GRANT: NAG1-1374
CONTRACT_GRANT: NAG1-1505
CONTRACT_GRANT: NAS1-19317
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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