首页 | 本学科首页   官方微博 | 高级检索  
     检索      

国内主力低速风洞大迎角实验的不确定度水平研究
引用本文:田学诗,司永昌.国内主力低速风洞大迎角实验的不确定度水平研究[J].实验流体力学,2007,21(1):73-76.
作者姓名:田学诗  司永昌
作者单位:中国航空工业空气动力研究院,哈尔滨,150001
摘    要:笔者将AGARD-AR-304不确定度评估方法推广到大迎角领域,给出计算低速风洞大(小)迎角实验不确定度的工程方法.相应的计算软件已成功地用于国内主力低速风洞实验的不确定度评估,完成了5座风洞8个模型大迎角实验的不确定度评估,给出了我国主力低速风洞大(小)迎角实验的不确定度水平.

关 键 词:低速风洞  大迎角  非对称涡  精度  不确定度
文章编号:1672-9897(2007)01-0073-04
收稿时间:2006-05-31
修稿时间:2006-07-26

The study on the test uncertainty level at high angles of attack for domestic capital low-speed wind tunnels
TIAN Xue-shi,SI Yong-chang.The study on the test uncertainty level at high angles of attack for domestic capital low-speed wind tunnels[J].Experiments and Measur in Fluid Mechanics,2007,21(1):73-76.
Authors:TIAN Xue-shi  SI Yong-chang
Institution:China Aerodynamic Research Institude of Aeronautics, Harbin 150001, China
Abstract:This report has conducted to extend the uncertainty assessment method of AGARD-AR-304 into the field of high angle of attack.The report presents an engineering method for calculating the uncertainty of experimental measurements for low speed wind tunnel tests at high or small angle of attack.Corresponding calculation software has been apllied to uncertainty assessments of tests for domestic capital low-speed wind tunnels successfully.Uncertainty assessments of tests on eight models in five wind-tunnels at high angles of attack are completed.Uncertainty level of fighter tests at high angles of attack for domestic capital low-speed wind tunnels is given.
Keywords:low-speed wind tunnel  high angle of attack  asymmetric vortices  precision  uncertainty
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号