本文选用不同的计算模型和网格数目在全流量域对NASA低速离心压气机进行了数值模拟,通过与实验数据的对比检验了计算结果的精度,为具有无叶扩压器结构的低压离心压气机确定了合理的计算方案.同时通过计算结果的观察和对比,分析了小流量下叶轮内部流场的部分变化特征.
参考文献
[1] | Hathaway M D;Chriss R M;Strazisar A J et al.Laser Anemometer Measurements of the Three-Dimensional Rotor Flow Field in the NASA Low-Speed Centrifugal Compressor[R].NASA TP-3257,1995. |
[2] | Hathaway M D;Chriss R M;Wood J R et al.Experimental and Computational Investigation of the NASA Low-Speed Centrifugal Compressor Flow Field[J].Journal of Turbomachinery,Transactions of the ASME,1993,115:527-542. |
[3] | Chriss R M;Hathaway M D;Wood J R .Experimental and Computational Results From the NASA Low-Speed Centrifugal Impeller at Design and Part Flow Conditions[R].ASME 94-GT-213,1994. |
[4] | Stein A;Niazi S;Sankar L N .Computational Analysis of Stall and Separation Control in Centrifugal Compressors[R].AIAA Paper 98-3296,1998. |
[5] | KANG S;Hirsch Ch .Effects of Flow Rate on the Development of Three-Dimensional Flow in NASA LSCC Impeller Based on Numerical Solutions[R].ISABE Paper99-7225,1999. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%