Effects of reynolds number on flow separation above generic half span transport aircraft model
The purpose of this study is to investigate the flow separation on UTM half model at 3 different Reynolds number which is 0.5 x 106, 1.0 x 106 and 1.5 x 106 which corresponds to speed, V = 20 m/s, 45 m/s and 65 m/s using pressure distribution method and flow visualization. The study was done to obse...
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| Format: | Article |
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2015
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