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超低速翼型升阻特性实验研究
引用本文:江善元,史卫成.超低速翼型升阻特性实验研究[J].南昌航空工业学院学报,2005,20(4):52-54,4.
作者姓名:江善元  史卫成
作者单位:南昌航空工业学院机械工程系,江西南昌330034
摘    要:本文介绍了用我们设计的一种翼型升阻特性实验台来做翼型升阻特性窘验的情况。包括实验方案、设备的主要结构和实验结果分析。通过本实验,可以测得某一特定实验机翼的升力特性和阻力特性。

关 键 词:翼型  升阻特性实验
文章编号:1001-4926(2005)03-0004-06
收稿时间:2005-07-05
修稿时间:2005-07-05

Study of superlow speed aerofoil lift-drag force characteristic test
JIANG Shan-yuan, SHI Wei-cheng.Study of superlow speed aerofoil lift-drag force characteristic test[J].Journal of Nanchang Institute of Aeronautical Technology(Natural Science Edition),2005,20(4):52-54,4.
Authors:JIANG Shan-yuan  SHI Wei-cheng
Institution:Dept. Of Mechanical Engineering, Nanchang Institute Of Aeronautical Technology, Nanchang 330034
Abstract:This paper introduces the experiment of the aerofoil llft - drag force characteristic test by using a kind of aerofoil lift - drag force characteristic test table designed by us. It includes the test project, the main structure of its instrument and the analysis of test result. It may obtain a special experiment aerofoil lift- drag Torce characteristic with this test.
Keywords:aerofoil  lift - drag force characteristic test
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