论文信息 - Orbital debris impact simulation using a parallel hybrid particle-element code

Orbital debris impact simulation using a parallel hybrid particle-element code

Simulations of three dimensional orbital debris impact problems, using a parallel hybrid particle-finite element code, show good agreement with experiment and good speedup in parallel computation. The simulations included single and multi-plate shields as well as aluminum and composite shielding materials, at an impact velocity of eleven kilometers per second.

Eric P. Fahrenthold | Ravishankar Ajjanagadde Shivarama | E. Fahrenthold

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