基于多核并行计算的超燃冲压发动机一维模型实时性研究  

Real-Time Research of Scramjet One Dimensional Model Simulation Based on Multi-Core Parallel Computation

作　　者：杨柳 史新兴[2] 刘小勇[1] 李岩[1] 苏承毅[1] 王明杰 YANG Liu;SHI Xin-xing;LIU Xiao-yong;LI Yan;SU Cheng-yi;WANG Ming-jie(Beijing Power Machinery Institute Beijing 100074,China;HIWING Technology Academy of CASIC,Beijing 100074,China)

机构地区：[1]北京动力机械研究所,北京100074 [2]中国航天科工飞航技术研究院,北京100074

出　　处：《推进技术》2022年第6期348-355,共8页Journal of Propulsion Technology

基　　金：国家科技重大专项(2017-V-0014-0066)。

摘　　要：在发动机控制系统设计中,为了缩短设计周期、降低研发成本,需要建立面向控制的、较为精确的、实时性高的超燃冲压发动机性能计算模型,以保证模型精度、提高计算速度为研究目标,基于多核高性能计算仿真平台,开展了面向控制的超燃冲压发动机一维模型实时性优化工作。运用简化计算流程、改进C语言程序、开拓缓存区等方法有效提高了一维模型计算速度。创新性地尝试了计算流体力学并行化方法,对隔离段和燃烧室一维模型进行结构分解。计算网格平衡分配至多个中央处理器,并借助核间数据通讯实现多核并行计算。与串行模型计算结果对比,七核并行计算模型性能参数偏差不超过0.1%,全工况仿真时间小于30ms,计算耗时较优化前缩短了75%以上。实时性优化后的多核并行模型计算精度高、速度快、收敛性好,可以作为超燃冲压发动机控制系统设计和半实物仿真验证平台。In the engine control system design,in order to shorten the design cycle of control system and reduce the cost of research and development,it is necessary to establish a good real-time scramjet engine model oriented to control. In order to ensure the model accuracy and improve the calculation speed,the real-time optimization of one-dimensional scramjet model for control was carried out based on the multi-core high-performance computing simulation platform. Firstly,the calculation speed of one-dimensional model was improved effectively by simplifying the calculation process,improving the C language program and expanding the cache area.Subsequently,the computational fluid dynamics parallelization method was tried innovatively,which decomposed the one-dimensional model of isolation section and combustor. The computing grids distributed multiple central processors in a balanced way and realized multi-core parallel computing with the help of inter-core data communication.Compared with the calculation results of the serial model,the deviation of the performance parameter of the seven-core parallel calculation model is less than 0.1% and the calculation time of the whole working condition is less than 30ms,and the calculation time is shortened by more than 75% compared with that before optimization. After real-time optimization,this parallel model has high computational accuracy,fast computation speed,good convergence,and can be used as a platform for scramjet control system design and hardware-inthe-loop simulation verification.

关 键 词：超燃冲压发动机 计算流体力学 空气动力学 并行计算 实时模型 

分 类 号：V231.3[航空宇航科学与技术—航空宇航推进理论与工程]