The applications of the luminescent pressure sensor FOP-1 in high-speed wind tunnel

被引：0

作者：

Zhang, YC ^{[1
]}

Zhang, R ^{[1
]}

Xing, HQ ^{[1
]}

Li, C ^{[1
]}

Zhou, JH ^{[1
]}

Cheng, HM ^{[1
]}

Chen, LS ^{[1
]}

Jin, XG ^{[1
]}

Du, JH ^{[1
]}

机构：

[1] Chinese Aerodynam Res Inst Aeronaut, Shenyang 110034, Peoples R China

来源：

OPTICAL TECHNOLOGY AND IMAGE PROCESSING FOR FLUIDS AND SOLIDS DIAGNOSTICS 2002 | 2002年 / 5058卷

关键词：

luminescent pressure sensor; pressure measurement; wind tunnel test;

D O I：

暂无

中图分类号：

TH7 [仪器、仪表];

学科分类号：

0804 ; 080401 ; 081102 ;

摘要：

The Optical Pressure Measurement (OPM) technique is a kind of practical pressure measurement in high-speed wind tunnel. The pressure data on the wing surface of an airplane model by both OPM technique and classic tap measurement technique in high-speed wind tunnel are given in this essay. The FOP-1 paint made in china was used in the OPM technique. The measuring results with the two techniques are discussed, and the performance of FOP-1 paint is proved to be good.

引用

页码：482 / 488

页数：7