| 采用新翼型的函道螺旋桨气动特性实验研究 |
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| 引用本文： | 上官云信,钟伯文,周瑞兴,郗忠祥,乔志德,陈上校,赵健,马涛.采用新翼型的函道螺旋桨气动特性实验研究[J].实验流体力学,1996(1). |
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| 作者姓名： | 上官云信 钟伯文 周瑞兴 郗忠祥 乔志德 陈上校 赵健 马涛 |
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| 作者单位： | 西北工业大学，上海７０８研究所 |
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| 摘 要： | 对国内、外螺旋桨翼型研制和发展的情况作了简单回顾后对分别采用ＮＰＵＰＲ翼型及ＮＡＣＡ－１６翼型设计的四种螺旋桨方案的气动设计方法作了简单说明，同时介绍了用这些方案进行风洞实验研究的主要结果，这些结果与计算结果相一致。此外，计算和实验结果表明：ＮＰＵＰＲ翼型设计的螺旋桨明显优于用ＮＡＣＡ－１６翼型设计的２方案，而用ＮＰＵＰＲ原翼型的Ｋ、Ｚ方案又明显优于应用户要求修型的１方案。
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| 关 键 词： | 新翼型 函道螺旋桨 气动设计 风洞实验 带动力实验 |
EXPERIMENTAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF SHROUDED PROPELLERS WITH NEW AEROFOIL |
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| Shangguan Yunxin,Zhong Bowen,Zhou Ruixing,Xi Zhongxian,Qiao Zhide.EXPERIMENTAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF SHROUDED PROPELLERS WITH NEW AEROFOIL[J].Experiments and Measur in Fluid Mechanics,1996(1). |
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| Authors: | Shangguan Yunxin Zhong Bowen Zhou Ruixing Xi Zhongxian Qiao Zhide |
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| Institution: | Shangguan Yunxin;Zhong Bowen;Zhou Ruixing;Xi Zhongxian;Qiao Zhide(Nothwestern Polytechnical University)Chen Shangxiao;Zhao Jian;Ma Tao(Shang-Hai's 708 Institute) |
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| Abstract: | This paper reviews briefly the developments of propeller section in domestic and abroad,and explains aerodynamical designing methods of four propeller schemes,which adopt the designing of NPU PR Section or NACA-16 aerofoil family.It also introduces the major results of these schemes which were obtained from wind tunnel testing.These experimental data from test agree with our computation numerical results.In addtion the results in both sides show that the propeller with NPU PR section is obviously superior to that(second scheme)with NACA-16 aerofoil family.Further more,the schemes of K and Z, which have propeller with NPU PR section,are superior to the first scheme, which is revised according to the user's requirements. |
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| Keywords: | new aerofoil shrouded propeller aerodynamical design wind tunnel testing powered testing |
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