作者: Shunsuke Koike , Hidemi Takahashi , Koichi Tanaka , Mitsutomo Hirota , Kenichi Takita
DOI: 10.2514/1.30962
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摘要: A correction method based on the Stokes drag law was developed for flow velocimetry using tracer particles. The present can be used to calculate corrected velocity from measured and its spatial gradient without need solve whole flowfield. Velocity measurement conducted sonic transverse injection into Mach 1.8 particle image velocimetry. applied field obtained data. data showed positions shapes of shock waves in region more clearly. peak downstream became closer theoretical values. jet streamlines calculated original were compared. went lower than those