航空学报 > 1982, Vol. 3 Issue (2): 100-104

薄附面层的测量技术研究

何中伟   

  1. 南京航空学院
  • 收稿日期:1981-05-01 修回日期:1900-01-01 出版日期:1982-06-25 发布日期:1982-06-25

STUDY ON THE MEASURING TECHNIQUE OF THIN BOUNDARY LAYERS

He Zhongwei   

  1. Nanjing Aeronautical Institute
  • Received:1981-05-01 Revised:1900-01-01 Online:1982-06-25 Published:1982-06-25

摘要: 本文介绍了一种自行设计和研制的可供测量薄附面层的微型传动器和附面层探针。传动器系以国产微型步进电机28 BF 001为主体设计的。它把电机转轴的角位移变为直线位移,其最小线位移速度每个脉冲为0.00625 mm;工作行程为5.0mm;具有良好的静态特性;其外径为28 mm,高度为50mm。结构简单。文中还介绍了二种薄附面层探针。 经在超音速气流中应用结果表明,传动器工作可靠,探针无抖动现象,能较准确地测出附面层速度分布。 在我国目前超音速风洞尺寸的实际条件下,设计一种用于测量薄附面层的微型传动器和附面层探针,很有实际意义。本文介绍了一种自行设计和研制的微型传动器和探针。

Abstract: A type of miniature driver with measuring probe 204-2 designed by ourselves for measurement of thin boundary layers is described. In the design the homemade miniature stepmotor 28BF001 serves as a main body. The driver is simple in construction (see Fig. 1) and reliable in operation. It transforms the angular displacement of the motor into linear displacement. Its minimum linear velocity is 0.00625mm per unit pulse, and its working travel is 5.0mm. The driver with an outside diameter of 28mm and height of 50mm has good static characteristics (Fig. 2). It is found that the experimental curve A, C extremely coincides with the theoretical curve B.Two types of measuring probes 204-2 are also presented in this paper. The outer height is 0.2mm and inner height 0.1mm for one probe tip, while for another they are 0.14mm and 0.07mm respectively. Both tips possess the same outer width of 1.0mm and the inner one of 0.6mm. The configurations of both probes are the same (see Fig. 3).The driver and the probes presented above have already been used for measuring the boundary layer parameters on the second cone of a supersonic intake working in supercritical conditions (Figs 4 and 5). The experiments were carried out in our supersonic intake tunnel with free-stream Mach numbers 1.97 and 2.10. The boundary layer profiles were shown in Fig. 6.By observing the movement of the probes during the experiments, it was proved that the driver and probes worked steadily in a supersonic flow without vibration, and the thin boundary layer profiles measured were quite correct.