复杂几何形状喷管内外三维流场的数值模拟  

Numerical simulation on internal and external flow fields of nozzle with complex geometry

作　　者：赵一鹗[1] 余少志[1] 

机构地区：[1]南京航空航天大学动力工程系,江苏南京210016

出　　处：《推进技术》2000年第3期30-33,共4页Journal of Propulsion Technology

摘　　要：研究了球面收敛矩形扩张的二元喷管 (SCFN)流场的数值模拟 ,为了有效地捕获激波与滑流面及较好地模拟分离 ,采用了 Roe格式、 MUSCL方法及 Venkatakrishnan限制器、 Spalart- Allmaras方程紊流模型。研究中给出了两个喷管模型四个流动状态的数值模拟结果。结果表明 ,除了有严重分离的流动情况以外 。The internal and external flow fields of SCFN 2 D nozzle was numerical simulated In order to capture the shockwaves effectively and simulate the separated flow fields better, Roe scheme and MUSCL approach,Venkatakrishnan limiter,Spalart Allmaras one equation turbulence model were used Some numerical results for four states of two SCFN models were presented It shows that very good computational results have been gotten with this arithmetic except the flow fields including serious separated domain

关 键 词：特型喷管 喷管气流 数值模拟 三维流场 

分 类 号：V435.11[航空宇航科学与技术—航空宇航推进理论与工程]