A new 48 d.o.f. quadrilateral shell element with variable-order polynomial and rational B-spline geometries with rigid body modes

Author:

Moore Carleton J.,Yang T. Y.,Anderson David C.

Publisher

Wiley

Subject

Applied Mathematics,General Engineering,Numerical Analysis

Reference30 articles.

1. and , Ed. Finite Elements for Thin Shells and Curved Members, Wiley, New York, 1976.

2. ‘The development and evaluation of matrix methods for thin shell structural analysis’, Report No. 8500-902011, Bell Aerosystems, Buffalo, New York (June 1966).

3. , and , ‘Dynamic analysis of shells using doubly-curved finite elements’, Proc. 2nd Conf. on Matrix Methods in Structural Mechanics, Air Force Flight Dynamics Laboratory, TR-68-150, Dayton, Ohio, Dec. 1969, pp. 185-212.

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