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NASA NTRS · 19920064111

Finite element approach for transient analysis of multibody systems

Abstract

A three-dimensional, finite element based formulation for the transient dynamics of constrained multibody systems with trusslike configurations is presented. A convected coordinate system is used to define the rigid-body motion of individual elements in the system. Deformation of each element is defined relative to its convected coordinate system. The formulation is oriented toward joint-dominated structures. Through a series of sequential transformations, the joint degree of freedom is built into the equations of motion of the element to reduce geometric constraints. Based on the derivation, a general-purpose code has been developed. Two examples are presented to illustrate the application of the code.

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BibTeXRIS

Wu, Shih-Chin, Chang, Che-Wei, Housner, Jerrold M.. 1992-08-01. Finite element approach for transient analysis of multibody systems. https://ntrs.nasa.gov/citations/19920064111

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