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NASA NTRS · 19900039763

A computational procedure for multibody systems including flexible beam dynamics

Abstract

A computational procedure suitable for the solution of equations of motions for flexible multibody systems has been developed. A fully nonlinear continuum approach capable of accounting for both finite rotations and large deformations has been used to model a flexible beam component. The beam kinematics are referred directly to an inertial reference frame such that the degrees of freedom embody both the rigid and flexible deformation motions. As such, the beam inertia expression is identical to that of rigid body dynamics. The nonlinear coupling between gross body motion and elastic deformation is contained in the internal force expression. Numerical solution procedures for the integration of spatial kinematic systems can be directily applied to the generalized coordinates of both the rigid and flexible components. An accurate computation of the internal force term which is invariant to rigid motions is incorporated into the general solution procedure.

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BibTeXRIS

Downer, J. D., Park, K. C., Chiou, J. C.. 1990-01-01. A computational procedure for multibody systems including flexible beam dynamics. https://ntrs.nasa.gov/citations/19900039763

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