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Overview of the DoD HPCMP Hypersonic Vehicle Simulation Initiative

机译:国防部HPCMP高超音速车辆仿真计划概述

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Simulation of hypersonic vehicles requires the inclusion of multiple scientific aspects that are not currently modeled appropriately, or are not included at all, in most simulation codes. These aspects include: combustion physics, turbulence and transition, fluid-thermal-structural interactions, non-equilibrium chemistry, shock-boundary layer interactions, and ablation. Without the inclusion of these aspects of hypersonic flight (either through physics-based prediction or appropriate modeling), simulation of hypersonic vehicles is deficient and cannot properly provide support to the development and acquisition of hypersonic vehicles. In order to improve the national capability in hypersonic vehicle RDT&E, a Hypersonic Vehicle Simulation Institute is being established by the DoD High Performance Computing Modernization Program. The institute will follow a multi-pronged, multi-year approach to address these shortcomings in hypersonic vehicle simulation.
机译:高超声速飞行器的仿真需要包含多个科学方面,这些方面目前在大多数仿真代码中尚未进行适当建模,或者根本没有包含。这些方面包括:燃烧物理学,湍流和过渡,流体-热-结构相互作用,非平衡化学,冲击边界层相互作用和消融。如果不包括高超音速飞行的这些方面(通过基于物理学的预测或适当的建模),高音速飞行器的模拟将是不足的,并且不能适当地为高音速飞行器的开发和获取提供支持。为了提高国家在超音速飞行器RDT&E方面的能力,美国国防部高性能计算现代化计划正在建立一个超音速飞行器仿真研究所。该研究所将采用多管齐下,多年的方法来解决高超声速车辆仿真中的这些缺点。

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