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Strategic Study of CAE >> 2009, Volume 11, Issue 11

Icing tunnel experimental study of the static pressure detector

School of Aeronautical Science and Engineering, Beihang University, Beijing 100191, China

Received: 2008-11-18 Available online: 2009-11-12 13:08:02.000

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Abstract

This work presented experimental approach of studying static pressure detector in an icing tunnel. The main topics are: the experimental items of the detector in the icing tunnel, the experimental conditions and the calibrating parameters measured in the experiment. According to the features of the icing tunnel, the experimental results of the detector and some suggestion for improvement were presented.

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References

[ 1 ] 裘燮纲,韩凤华.飞机防冰系统[M].北京航空专业教材编审组出版,1985

[ 2 ] Gern F H.Aerodynamic, thermal, and anti -icing analysis of the IMFP integrated air data sensor[ R] .AIAA -2004 -2138 , 2004

[ 3 ] 航空器适航司.中国民用航空规章第25部—运输类飞机适航标准第三次修订版[M].北京:中国民用航空总局,2001

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