Pressure field measurements on large-scale propeller blades using pressure-sensitive paint

被引:1
作者
Wei, Chunhua [1 ]
Jiao, Lingrui [2 ,3 ]
Tong, Fan [1 ]
Chen, Zhengwu [1 ]
Liu, Yingzheng [2 ,3 ]
Peng, Di [2 ,3 ]
机构
[1] China Aerodynam Res & Dev Ctr, Mianyang 621000, Sichuan, Peoples R China
[2] Shanghai Jiao Tong Univ, Sch Mech Engn, Key Lab, Educ Minist Power Machinery & Engn, Shanghai 200240, Peoples R China
[3] Shanghai Jiao Tong Univ, Gas Turbine Res Inst, Shanghai 200240, Peoples R China
基金
中国国家自然科学基金;
关键词
Pressure-sensitive paint; Pressure distribution; Propeller blade; PREDICTION; PSP;
D O I
10.1007/s10409-021-09048-1
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Pressure-sensitive paint (PSP) is a global pressure measurement technique. Compared with pressure transducers, PSP has significant advantages such as high spatial resolution and a lack of contact when applied to fast-rotating blades. However, due to the limitations of other pressure measurement techniques, the validation of PSP measurements on fast-rotating blades is generally difficult. In this work, a comprehensive study including PSP measurement, force balance measurement, and simulation was conducted on a 1 m-diameter propeller at the China Aerodynamic Research and Development Center. First, our computational fluid dynamics (CFD) code was validated by comparing the calculated aerodynamic thrust with the results from force balance measurements. Then, the pressure distributions on the propeller blade obtained by PSP were carefully compared with the CFD results under different working conditions. The results of PSP measurements, force balance measurements, and CFD showed good agreement, and the PSP measurement errors were estimated to be less than 5% of the dynamic pressure at the blade tip. Finally, the variations in pressure distribution under different rotating speeds and free-stream velocities were discussed.
引用
收藏
页数:11
相关论文
共 25 条
[1]   PREDICTION OF ADVANCED PROPELLER NOISE IN THE TIME DOMAIN [J].
FARASSAT, F .
AIAA JOURNAL, 1986, 24 (04) :578-584
[2]   EXPERIMENTAL AND NUMERICAL STUDY OF THE PROPELLER FIXED WING INTERACTION [J].
FRATELLO, G ;
FAVIER, D ;
MARESCA, C .
JOURNAL OF AIRCRAFT, 1991, 28 (06) :365-373
[3]   Review of measurement techniques for unsteady helicopter rotor flows [J].
Gardner, A. D. ;
Wolf, C. C. ;
Raffel, M. .
PROGRESS IN AEROSPACE SCIENCES, 2019, 111
[4]   Fast Pressure-Sensitive Paint for Flow and Acoustic Diagnostics [J].
Gregory, James W. ;
Sakaue, Hirotaka ;
Liu, Tianshu ;
Sullivan, John P. .
ANNUAL REVIEW OF FLUID MECHANICS, VOL 46, 2014, 46 :303-330
[5]   Motion-deblurred, fast-response pressure-sensitive paint on a rotor in forward flight [J].
Juliano, Thomas J. ;
Disotell, Kevin J. ;
Gregory, James W. ;
Crafton, Jim ;
Fonov, Sergey .
MEASUREMENT SCIENCE AND TECHNOLOGY, 2012, 23 (04)
[6]   Single-shot, lifetime-based pressure-sensitive paint for rotating blades [J].
Juliano, Thomas J. ;
Kumar, Pradeep ;
Peng, Di ;
Gregory, James W. ;
Crafton, Jim ;
Fonov, Sergey .
MEASUREMENT SCIENCE AND TECHNOLOGY, 2011, 22 (08)
[7]  
Klein C., 2014, FLUID MECH MULTIDISC, V124, P535
[8]  
Kulesh V. P., 2006, SOC PHOTOOPT INSTRUM
[9]   Unsteady skin-friction field estimation based on global luminescent oil-film image analysis [J].
Lee, Taekjin ;
Lee, Chungil ;
Nonomura, Taku ;
Asai, Keisuke .
JOURNAL OF VISUALIZATION, 2020, 23 (05) :763-772
[10]  
Mitchell G., 1982, 19821119 AIAA