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一种涵道螺旋桨的简便设计方法
引用本文:高永卫,黄灿金,魏闯.一种涵道螺旋桨的简便设计方法[J].航空工程进展,2013,4(3):352-357.
作者姓名:高永卫  黄灿金  魏闯
作者单位:西北工业大学航空学院,西安,710072
摘    要:由于涵道和螺旋桨互相干扰的复杂性,通常涵道螺旋桨的设计需要较多经验和较长时间。提出一种将动量定理、轴流式通风机相似理论和旋转机械叶素理论相结合的工程方法,该方法应用在涵道螺旋桨初步设计阶段,可快速确定桨叶和涵道初始外形。首先根据动量理论计算通过桨盘的流量,再由轴流通风机相似理论确定桨盘直径与轮毂比,然后运用叶素理论设计桨叶的几何形状。风洞实验结果表明:该设计方法实用、有效,从而可以加快涵道螺旋桨设计过程。

关 键 词:涵道螺旋桨  动量理论  相似理论  叶素理论  桨叶设计

A Simple Approach to the Design of Ducted Propeller
Gao Yongwei , Huang Canjin , Wei Chuang.A Simple Approach to the Design of Ducted Propeller[J].Advances in Aeronautical Science and Engineering,2013,4(3):352-357.
Authors:Gao Yongwei  Huang Canjin  Wei Chuang
Institution:(School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China)
Abstract:Ducted propeller design is often by rule of thumb, and requires a long time for the complexity of the mutual interaction between duct and propeller. A simple method, which is combined with momentum theory, the axial fan similarity and the blade-element theory, is proposed for the purpose of designing the blades and duct during ducted propeller preliminary design stage. First, the mass flow through the propeller disk is calcu- lated using the momentum theory. Then the fan diameter and hub diameter are estimated by similarity of axial fan introduced by the authors. Finally the blade primary geometry is designed on the basis of blade element the- ory. To verify feasibility of this method, a ducted propeller is manufactured and tested in NF-3 low speed wind tunnel. The result shows that the method is useful and effective, and can accelerate ducted propeller design pro- cedure.
Keywords:ducted propeller  momentum theory  similarity theory  blade element theory  blade design
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