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A Lagrangian model for debris cloud dynamics simulation
Authors:E P Fahrenthold
Affiliation:

Department of Mechanical Engineering, University of Texas, Austin, TX 78712, USA

Abstract:A new modeling approach has been developed for computer simulation of hypervelocity impacts on multi-plate orbital debris shields. This approach links an Eulerian finite difference code for shield perforation calculations to a Lagrangian finite element code for debris cloud evolution simulations. Mixture theory is used to account for the presence of void space in the debris cloud.
Keywords:
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