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作 者:周强[1] 刘波[1] 高丽敏[1] 陈柳生[1] 史淼[1]
机构地区:[1]西北工业大学动力与能源学院
出 处:《Chinese Journal of Aeronautics》2009年第2期138-144,共7页中国航空学报(英文版)
基 金:National Natural Science Foundation of China (50476071, 10577020)
摘 要:Global pressure distribution on the suction surface of a single vane in a transonic cascade wind tunnel is measured with the help of intensity-based pressure-sensitive paint (PSP) technique using a type of temperature-insensitive fluorescent paint and a self-made measurement system. This measurement is conducted at the outlet of the cascade wind tunnel at the Mach numbers 0.3 and 0.4, attack angle about –20°, ambient pressure 95.4 kPa and temperature 15 °C. The vane under study owns a large camber angle of ...Global pressure distribution on the suction surface of a single vane in a transonic cascade wind tunnel is measured with the help of intensity-based pressure-sensitive paint (PSP) technique using a type of temperature-insensitive fluorescent paint and a self-made measurement system. This measurement is conducted at the outlet of the cascade wind tunnel at the Mach numbers 0.3 and 0.4, attack angle about –20°, ambient pressure 95.4 kPa and temperature 15 °C. The vane under study owns a large camber angle of ...
关 键 词:TURBOMACHINERY pressure measurement pressure-sensitive paint pressure distribution cascade wind tunnel suction surface of vane image registration
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