北京航空航天大学 航空发动机气动热力重点实验室,北京,100083
Published:2008
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LI Qing-liang, LIU Bao-jie. Modification of the turbulence model of DENTON code[J]. 2008, 23(5).
DOI:
LI Qing-liang, LIU Bao-jie. Modification of the turbulence model of DENTON code[J]. 2008, 23(5). DOI:
改进了DENTON程序所使用的混合长度模型
使之能够适应壁面发展以及有适度分离流动的情况
并减少对经验的依赖.通过对NASARotor67转子和Rotor37转子的对比计算分析
验证了改进的混合长度模型能够进一步提高计算的可靠性
并且计算时间增加很少
保持了DENTON程序计算速度快的优势.
The mixing length model of DENTONcode was modified to make it fit the development of boundary layer and moderate scale separation
and also reduce the dependence on experience.By comparative calculation and analysis of NASA Rotor 67 and NASA Rotor 37
it shows that the modified model could further improve the computational reliability with little increase of CPUtime
and also maintain the fast advantage of DENTONcode.
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