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三角翼飞机气动压力测量试飞技术研究
引用本文:陈怦,余俊雅,张德元,孟建文,黄文静.三角翼飞机气动压力测量试飞技术研究[J].飞行力学,2001,19(3):56-59.
作者姓名:陈怦  余俊雅  张德元  孟建文  黄文静
作者单位:中国飞行试验研究院飞机所
摘    要:回顾了气动压力测量技术的国内外发展现状,介绍了三角翼表面压力飞行试验测量技术、试飞总体方案及实施方法,并对飞机试验情况进行了,给出了不同速度下飞机机翼表面压力分布试飞结果和飞机活动翼面的压力分布测量结果,试飞结果表明,机翼蒙皮直接改装测量孔和测压带方法均能有效测量机翼表达压力分布。

关 键 词:压力测量  压力分布  三角翼飞机  飞行试验  机翼蒙皮
文章编号:1002-0853(2001)03-0056-04
修稿时间:2001年5月9日

Flight test research of aerodynamics pressure measurement technique for a delta-wing aircraft
CHEN Peng,YU Jun-ya,ZHANG De-yuan,MENG Jian-wen,HUANG Wen-jing.Flight test research of aerodynamics pressure measurement technique for a delta-wing aircraft[J].Flight Dynamics,2001,19(3):56-59.
Authors:CHEN Peng  YU Jun-ya  ZHANG De-yuan  MENG Jian-wen  HUANG Wen-jing
Abstract:This paper briefly looks back the development of aerodynamics pressure measurement technique. With introduced the process of the delta-wing aircraft flight test, the testing-program determining technique and test-flying method is described. The date process with some pressure distribution results determined on wing-surface and movable surface from test is also provided. The flight test results show that the Stripe-A-Tube method is as more effective as measurement that transform hole of static pressure on wing surface.
Keywords:pressure measurement  pressure distribution  delta-wing aircraft  flight test
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