POROUS PRESSURE-SENSITIVE PAINT FOR MEASUREMENT OF UNSTEADY PRESSURES IN TURBOMACHINERY
作者： James Gregory
DOI: 10.2514/6.2004-294
关键词: Acoustics 、 Impeller 、 Turbomachinery 、 Turbocharger 、 Structural engineering 、 Flutter 、 Engineering 、 Stator 、 Gas compressor 、 Pressure-sensitive paint 、 Pressure measurement
摘要: This work details the development and application of porous pressure-sensitive paint (PSP) for measuring unsteady surface pressures in turbomachinery. The advantages PSP over conventional methods include global pressure measurement, fast response time, instrumentation thin turbomachinery components that are otherwise difficult or impossible to instrument. In this paper, development, calibration, discussed. Porous formulations were developed ensure times good adhesion characteristics rotating parts. Experimental such as phase-locking image registration acquire quality data. Dynamic calibrations with a fluidic oscillator performed, indicating have time up 40 kHz. For application, inlet wall impeller blades turbocharger compressor painted fast-responding polymer/ceramic PSP. was operated at 100,000 rpm, corresponding blade-passage frequency (BPF) 10 Even high speed BPF, able resolve distributions about blade. addition, flow blockage created induce an distortion on compressor. 1.67 kHz blade loading. Potential applications testing evaluations rotor/stator interaction, flutter, distortion, stall, surge.
sci-hub.se 参考文章(22)
T. Liu, J. Sullivan, S. Torgerson, Rotor Blade Pressure Measurement in a Rotating Machinery Using Pressure and Temperature Sensitive Paints Propulsion and energetics panel. Symposium. ,(1998)
Surya Raghu, Feedback-free fluidic oscillator and method ,(1999)
K. Asai, H. Kanda, C.T. Cunningham, R. Erausquin, J.P. Sullivan, Surface pressure measurement in a cryogenic wind tunnel by using luminescent coating international congress on instrumentation in aerospace simulation facilities. ,vol. 1997, pp. 105- 114 ,(1997) , 10.1109/ICIASF.1997.644671
James H Bell, Edward T Schairer, Lawrence A Hand, Rabindra D Mehta, Surface Pressure Measurements Using Luminescent Coatings Annual Review of Fluid Mechanics. ,vol. 33, pp. 155- 206 ,(2003) , 10.1146/ANNUREV.FLUID.33.1.155
Ganesh Raman, Surya Raghu, Cavity Resonance Suppression Using Miniature Fluidic Oscillators AIAA Journal. ,vol. 42, pp. 2608- 2612 ,(2004) , 10.2514/1.521
J. H. Bell, B. G. McLachlan, Image registration for pressure-sensitive paint applications Experiments in Fluids. ,vol. 22, pp. 78- 86 ,(1996) , 10.1007/BF01893308
Alan E. Baron, J. D. S. Danielson, Martin Gouterman, Jiang River Wan, James B. Callis, Blair McLachlan, Submillisecond response times of oxygen‐quenched luminescent coatings Review of Scientific Instruments. ,vol. 64, pp. 3394- 3402 ,(1993) , 10.1063/1.1144310
Jan Lepicovsky, PSP Measurement of Stator Vane Surface Pressures in a High Speed Fan Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education. ,(1998) , 10.1115/98-GT-499
C. H. Sieverding, T. Arts, R. Dénos, J.-F. Brouckaert, Measurement techniques for unsteady flows in turbomachines Experiments in Fluids. ,vol. 28, pp. 285- 321 ,(2000) , 10.1007/S003480050390
Tianshu Liu, B. T. Campbell, S. P. Burns, J. P. Sullivan, Temperature- and Pressure-Sensitive Luminescent Paints in Aerodynamics Applied Mechanics Reviews. ,vol. 50, pp. 227- 246 ,(1997) , 10.1115/1.3101703