过膨胀状态下轴对称收-扩喷管内外流场计算及分析

黄宏艳; 王强

过膨胀状态下轴对称收-扩喷管内外流场计算及分析

黄宏艳,
王强

北京航空航天大学能源与动力工程学院, 北京 100083

计量
- 文章访问数: 1424
- HTML浏览量: 0
- PDF量: 408
- 被引次数: 0
出版历程
- 收稿日期: 2006-06-23
- 修回日期: 2006-10-10
- 刊出日期: 2007-07-28

Numerical investigation on internal and external flows for axisymmetric convergent-divergent nozzles on over-expansion state

School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

摘要

摘要: 轴对称收-扩喷管在过膨胀状态下工作时, 喷管内部将产生强烈的激波以及附面层分离, 流态非常复杂.计算实践表明, 应用广泛采用的重整化群(RNG)k-ε湍流模型, 并结合标准壁面函数对其进行数值模拟时, 误差较大.针对标准壁面函数的不足, 采用增强型壁面函数处理固体壁面附近的流动, 对轴对称收-扩喷管的内外流场进行了数值模拟, 并与试验数据进行了分析比较.结果表明:增强型壁面函数更加适合处理此类存在强逆压梯度导致附面层分离的问题.
- 航空、航天推进系统 /
- 壁面函数 /
- 流动特性 /
- 数值模拟 /
- 过膨胀 /
- 附面层分离
Abstract: When a axisymmetric convergent-divergent nozzle work at an over-expansion state,the strong shock wave and layer separation appear in the interior of the nozzle and the flow characteristic is very complex.The computed results were compared unfavorably with experimental data when adopting RNG k-ε turbulent model with standard wall functions.A wall treatment that combines a two-layer model with enhanced wall functions was employed in the numerical simulation and it was in good agreement with the experimental data.It is suggested that this enhanced wall treatment is more effective to deal with the problem of severe pressure gradients leading to boundary layer separations.
- aerospace propulsion system /
- wall functions /
- flow characteristic /
- numerical simulation /
- over-expansion /
- boundary layer separations

HTML

参考文献(9)

[1]	Lee C G T,Edwin E Jr.Experimental and analytical investigation of axisymmetric supersonic cruise nozzle geometry at Math numbers from 0.60 to 1.30[R].NASA TP 1953,1981.
[2]	Carlson J R.Computational prediction of isolated performance of an axisymmetric nozzle at Maeh number 0.90[R].NASA TM-4506.1994.
[3]	Leonard B P.A stable and accurate convective modeling procedure based on quadratic upstream interpolation[J].Computer Methods in Applied Mechanics and Engineering,1979,19:59-98.
[4]	Yakhot V,Orzag S A.Renormalization group analysis of Turbulence:basic theory[J].Journal of Scientific Computing,1986,1:3-11.
[5]	陶文铨.数值传热学[M].西安:西安交通大学出版社,2001.
[6]	Launder B E,Spalding D B.The numierical computation of turbulent flows[J].Computer Methods in Applied Meehanies and Engineering,1974,3:269-289.
[7]	Kader B.Temperature and concentration profiles in fully turbulent boundary layers[J].Journal of Heat Mass Transfer,1981,24(9):1541-1544.
[8]	White F,Christoph G.A simple new analysis of compressible turbulent skin friction under arbitrary conditions[R].February 1971,Technical Report AFFDL-TR-70-133.
[9]	Huang P,Bradshaw P,Coakley T.Skin friction and velocity profile family for compressible turbulent boundary layers[J].AIAA Journal,1993,31(9):1600-1604.