Pressure Measurement on Suction Surface of a Single Vane Using Pressure-sensitive Paint

Chinese Journal of Aeronautics

Volumn 22, Issue 2, 2009, Pages 138-144

  Zhou, Qiang ^a   Liu, Bo ^a   Gao, Limin ^a   Chen, Liusheng ^b   Shi, Miao ^b  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^b INSTITUTE OF CHEMISTRY   (China)

Author keywords

cascade wind tunnel; image registration; pressure distribution; pressure measurement; pressure sensitive paint; suction surface of vane; turbomachinery

Indexed keywords

AMBIENT PRESSURES; ATTACK ANGLES; CAMBER ANGLES; CASCADE WIND TUNNEL; FLUORESCENT PAINTS; INTENSITY-BASED; MAXIMUM ERRORS; MEASUREMENT SYSTEMS; OPERATING SEQUENCES; PRESSURE PORTS; PRESSURE-SENSITIVE PAINT; STATIC PRESSURES; STEEL PLATES; SUCTION SURFACE OF VANE; TEMPERATURE-INSENSITIVE;

AERODYNAMICS; IMAGE REGISTRATION; MACH NUMBER; MEASUREMENTS; PAINT; PRESSURE DISTRIBUTION; PRESSURE MEASUREMENT; PRESSURE SENSORS; STEEL; SUBMERSIBLE PUMPS; TUNNELS; TURBOMACHINERY; WIND TUNNELS;

LUMINOUS PAINT;

EID: 64849115839     PISSN: 10009361     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1000-9361(08)60079-5     Document Type: Article

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