某高空螺旋桨气动特性数值模拟与风洞试验  

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

作　　者：王裕夫[1] 刘振国[1] 陶国权[1] 

机构地区：[1]北京航空航天大学航空科学与工程学院,北京100191

出　　处：《北京航空航天大学学报》2013年第8期1102-1105,共4页Journal of Beijing University of Aeronautics and Astronautics

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.High altitude propeller was studied. The three-dimensional Navier-Stokes equations were used to simulate the complex flow around a high altitude propeller and its aerodynamic characteristics were analyzed, in which the k-ε turbulence model was used. In accordance with similarity criteria such as equal Reynolds number and equal advanced ratio, the scaled model test of high altitude propeller was carried out. The simulation results are in good agreement with test results. The feasibility of the numerical simulation method for aerodynamic characteristics calculation of high altitude propeller is proved, and provides reference basis for the design and test of high altitude propellers.

关 键 词：高空螺旋桨 数值模拟 相似准则 地面风洞试验 

分 类 号：O355[理学—流体力学]