Comparison of Unsteady Pressure-Sensitive Paint Measurement Techniques

被引:14
作者
Fang, Shuo [1 ]
Long, Samuel R. [1 ]
Disotell, Kevin J. [1 ]
Gregory, James W. [1 ]
Semmelmayer, Frank C. [2 ]
Guyton, Robert W. [2 ]
机构
[1] Ohio State Univ, Dept Mech & Aerosp Engn, Columbus, OH 43235 USA
[2] USAF, Res Lab, Expt Fluid Branch, Aeronaut Sci Div AFRL RBAX, Wright Patterson AFB, OH 45433 USA
关键词
REYNOLDS-NUMBERS; SPHERE;
D O I
10.2514/1.J051167
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The current work focuses on the development and application of fast-responding polymer/ceramic pressure-sensitive paint (PSP) as an advanced optical surface pressure measurement technique for unsteady flowfields in large-scale wind tunnels. Three different data acquisition methods for PSP are evaluated and compared: phase averaging, real-time (high-speed) imaging, and single-shot lifetime imaging. All three techniques were applied to the measurement of the time-resolved, global surface pressure distribution on a hemispherical dome in Mach 0.6 freestream flow at a total pressure of 71.8 kPa, where the Reynolds number based on dome diameter (0.254 m) was 2.4 x 10(6). At this flow condition, a predominant shear layer oscillating at 400 Hz over the test model was detected by pressure transducer measurement, providing an appropriate trigger for the PSP optical instrumentation. In the phase-averaging technique, pulsed LED arrays were phase-locked to the shear-layer frequency, and a long camera exposure time captured the pressure distribution over many phase-averaged cycles. In the real-time approach, high-intensity continuous LED illumination was paired with a high-speed camera operating at a frame rate of 10 kHz to capture the pressure distribution without any image averaging. In the lifetime-based single-shot approach, instantaneous pressure information was acquired by exciting the paint with pulsed laser energy and ratioing two exposure gates, which covered the luminescent lifetime decay of the luminophore molecules resulting from each excitation pulse. An assessment of the three methods is presented, with the benefits and disadvantages of each technique evaluated through the ease study of the hemispherical dome.
引用
收藏
页码:109 / 122
页数:14
相关论文
共 41 条
[1]  
[Anonymous], 35 AIAA FLUID DYN C
[2]  
[Anonymous], 2010, THESIS OHIO STATE U
[3]  
Asai K., 2000, 21 AIAA AER MEAS TEC
[4]  
Asai K., 1997, 17 INT C INSTR AER S, P105
[5]  
Asai K., 2011, AIAA 2011-0847
[6]   Surface pressure measurements using luminescent coatings [J].
Bell, JH ;
Schairer, ET ;
Hand, LA ;
Mehta, RD .
ANNUAL REVIEW OF FLUID MECHANICS, 2001, 33 :155-206
[7]   Image registration for pressure-sensitive paint applications [J].
Bell, JH ;
McLachlan, BG .
EXPERIMENTS IN FLUIDS, 1996, 22 (01) :78-86
[8]  
Bencic T. J, 2001, 39 AIAA AER SCI M EX
[9]  
Covington M, 2007, DIGITAL SLR ASTROPHO, P22
[10]   Pressure sensitive paint systems for pressure distribution measurements in wind tunnels and turbomachines [J].
Engler, RH ;
Klein, C ;
Trinks, O .
MEASUREMENT SCIENCE AND TECHNOLOGY, 2000, 11 (07) :1077-1085