摘要
本文在并行计算环境下对火箭发动机湍流两相燃烧流场进行了数值模拟 ,用并行系统分析模型对机器的性能和应用程序进行了研究 ,通过测试表明预测和实测结果相符 。
The two phase turbulent combustion flow fields were simulated under parallel computation. The parallel machine performance and applied program were studied with the model of parallel machine analyzed model. The predicted and real tested results were almost the same. The modified parallel program had high parallel efficiency.
出处
《空气动力学学报》
CSCD
北大核心
2002年第z1期34-38,共5页
Acta Aerodynamica Sinica
基金
国家自然科学基金重点资助项目 (6 99330 30 )
86 3- 30 6主题资助项目
关键词
并行计算
火箭发动机
并行系统分析模型
parallel computation
rocket engine
parallel machine analyzed model
