## 留言板

 引用本文: 王裕夫, 刘振国, 陶国权等 . 某高空螺旋桨气动特性数值模拟与风洞试验[J]. 北京航空航天大学学报, 2013, 39(8): 1102-1105.
Wang Yufu, Liu Zhenguo, Tao Guoquanet al. Numerical simulation of high altitude propeller’s aerodynamic characteristics and wind tunnel test[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(8): 1102-1105. (in Chinese)
 Citation: Wang Yufu, Liu Zhenguo, Tao Guoquanet al. Numerical simulation of high altitude propeller’s aerodynamic characteristics and wind tunnel test[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(8): 1102-1105. (in Chinese)

• 中图分类号: O355

## Numerical simulation of high altitude propeller’s aerodynamic characteristics and wind tunnel test

• 摘要: 以某高空螺旋桨为研究对象,利用k-ε湍流模型,采用三维Navier-Stokes方程,并通过数值计算模拟该螺旋桨的复杂绕流,分析其气动特性.按照等雷诺数等前进比准则,进行了该螺旋桨地面缩比风洞试验.经过比较发现,计算结果与试验结果吻合良好.验证了数值模拟计算高空螺旋桨气动特性的正确性,为高空螺旋桨的设计和试验提供参考依据.

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##### 出版历程
• 收稿日期:  2012-09-24
• 修回日期:  2012-11-26
• 网络出版日期:  2013-08-30

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