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无人机螺旋桨性能工程检验方法研究

谢辉 王力 张琳

航空工程进展Issue(4):418-422,5.
航空工程进展Issue(4):418-422,5.

无人机螺旋桨性能工程检验方法研究

Research on Checkout Method of UAV’s Propeller

谢辉 1王力 1张琳1

作者信息

  • 1. 西安爱生技术集团公司飞行设计研究室,西安 710065
  • 折叠

摘要

Abstract

The method of measuring rotate speed with piston motor is used to judge the aerodynamic capability of manufactured propellers in engineering .But the method is not good in fact .Accordingly ,in base of results of rotate speed measured by piston motor in ground condition ,the aerodynamic characteristics of the same type of propeller in different velocities and rotate speeds ,such as efficiency ,thrust coefficient and power coefficient ,are measured in low‐speed wind tunnel test ,and flight emulation method is used to compute flight capabilities of the same UAV after getting the test data .Results show that the efficiency ,thrust coefficient and power coefficient of propeller are not directly in relation with the rotate speed measured in ground condition with piston motor by comparing the results in wind tunnel test and computation .Consequently ,the method of measuring rotate speed with piston motor is not crucial but only referenced in checkout method of UAV’s propeller .

关键词

无人机/螺旋桨/检验/转速/风洞试验

Key words

UAV/propeller/checkout/rotate speed/wind tunnel test

分类

航空航天

引用本文复制引用

谢辉,王力,张琳..无人机螺旋桨性能工程检验方法研究[J].航空工程进展,2014,(4):418-422,5.

航空工程进展

OACSCD

1674-8190

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