系统仿真学报 ›› 2019, Vol. 31 ›› Issue (9): 1733-1740.doi: 10.16182/j.issn1004731x.joss.19-0406

• 专栏:复杂系统建模与仿真 •    下一篇

基于HPC的多学科多物理场耦合虚拟飞行试验方法

铁鸣, 于盈, 张星, 王建林   

  1. 空间物理重点实验室,北京 100076
  • 收稿日期:2019-07-31 修回日期:2019-08-03 发布日期:2019-12-12
  • 作者简介:铁鸣(1976-),男,回族,辽宁沈阳,博士,研究员,研究方向为复杂系统建模与仿真、智能建模与优化。
  • 基金资助:
    国家自然科学基金(61773068),国家重点研发计划(2018YFB1701600)

HPC-based Virtual Flight Test Method for Multidisciplinary Multiphysical Field Coupling

Tie Ming, Yu Ying, Zhang Xing, Wang Jianlin   

  1. Key Laboratory of Space Physics, Beijing 100076, China
  • Received:2019-07-31 Revised:2019-08-03 Published:2019-12-12

摘要: 虚拟飞行试验是临近空间飞行器总体性能验证补充手段。多物理场耦合建模仿真的复杂性对虚拟试验精度和效率都形成挑战,已成为系统仿真领域的一个经典问题。基于此,建立了多物理场耦合仿真模型,提出多物理场耦合的高效并行仿真架构多专业异构CAE模型协同运行方法,研究了任务级、算法级混合大规模并行仿真技术,构建了基于高性能计算机High performance computer,HPC)的虚拟飞行试验系统Flight system testbed,FST),显著提高了虚拟飞行试验效率,对飞行器总体设计水平的提升具有重要意义。

关键词: 虚拟飞行试验系统, 临近空间飞行器, 多物理场耦合, 高性能计算, 总体性能

Abstract: Multidisciplinary simulation based on virtual flight system testbed (FST) will become an alternative way for the overall performance validation of near space hypersonic vehicles (HSV). The complexity of multi-physical field coupled modeling and simulation challenges the accuracy and efficiency of virtual experiment. Therefore, a multi-physical-field coupling simulation model is established. The architecture of HPC-FST is explicitly expounded for large-scale parallel multidisciplinary virtual flight tests and multi-physics coupling simulation of whole vehicle. Moreover, an integration algorithm is developed for heterogeneous CAE models in collaborative simulation. A HPC based parallel virtual flight test method with a task-level and algorithm-level hybrid large-scale parallel simulation technology is developed for whole flight envelope simulation, and a large-scale parallel simulation algorithm is proposed for efficient simulation of aerodynamic flow field. Based on the supercomputer, HPC-FST is a high efficient platform for overall performance validation of HSV, which will reduce development cost as well as improve integrated design capability.

Key words: virtual flight system testbed, near space vehicle, multi-physical coupling, high performance computing, overall performance

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