飞行器亚跨超声速流气动力并行计算研究  

Parallel numerical calculations for subsonic transonicand supersonic flows of vehicles

作　　者：徐庆新[1] 张玉伦[1] 

机构地区：[1]中国空气动力研究与发展中心,四川绵阳621000

出　　处：《空气动力学学报》2002年第z1期52-58,共7页Acta Aerodynamica Sinica

基　　金：国防科学技术预先研究基金资助项目;国家自然科学基金 (86 3- 30 6主题 )资助项目

摘　　要：隐格式并行求解是计算流体力学并行算法研究的难点 ,本文针对分布式存储并行处理系统 ,在异构编程PVM环境下 ,采用“局部隐”方法 ,使用发送 /接收数据结构和自动剖分等技术 ,有效地实现了对飞行器亚跨超声速流气动力数值模拟串行程序的并行化改造 ,保证了并行计算结果与串行结果的一致性。该方法具有简单实用。Parallel computations for implicit scheme is very difficult in parallel algorithms of computational fluid dynamics. This paper adopts a so-called local implicit method with the technology of sending/receiving data structure and automatic partition. It effectively realizes the parallel computations for subsonic, transonic and supersonic flows of vehicles under parallel distributed network system with PVM platform, which the parallel results are consistent with serial results. It is a simple and applied method with a high parallel efficiency. The parallel soft has a good transplantability and a far-ranging applications.

关 键 词：并行计算 局部隐格式 跨声速流 

分 类 号：V211.3[航空宇航科学与技术—航空宇航推进理论与工程]