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实验的情况,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。
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.
出处
《南昌航空工业学院学报》
CAS
2005年第4期52-54,4,共4页
Journal of Nanchang Institute of Aeronautical Technology(Natural Science Edition)
关键词
翼型
升阻特性实验
aerofoil
lift - drag force characteristic test