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Experimental Studies of Dimpled Surface Effect on the Performance of Linear Cascade under Different Incidence Angles

机译:不同入射角下凹面效应对线性叶栅性能的实验研究

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In this paper, preliminary experiments were conducted to investigate the effect of dimpled surface on the performance of linear cascade. Two dimple configurations with a diameter of 1.0mm and a depth-diameter ratio of 0.2, which were located in 30%-60% and 75%-95% axial chord lengths of suction side respectively, were studied to validate their effectiveness in reducing total pressure loss. Incidence angles of -5.3°, 0°, 5.3°, 7.5°, 10° and inlet Mach number of 0.4 were used in each experiment with 1.5% Tu. Total pressure loss coefficients and blade loading force measurements were made on the dimpled blades by a mini 5-hole pressure probe and compared to the smooth blades. The experimental results show that the reduction of the total pressure loss coefficients of dimpled blades is obvious at the incidence angle of 0°, 5.3°, and 7.5°, and the change of the total pressure loss coefficients of dimpled blades is very slight at the incidence angle of -5.3°, and 10°. In addition, there exists a slight increase of loading force with dimpled blades. The comparison results also indicate that dimples on 30%-60% of suction side is more effective in loss reduction than that on 75%-95% of suction side at all incidence angles.
机译:在本文中,进行了初步实验以研究凹坑表面对线性级联性能的影响。研究了两种分别位于吸力侧轴向弦长的30%-60%和75%-95%的直径为1.0mm且深径比为0.2的凹窝构型,以验证它们在减小总负重方面的有效性。压力损失。每个实验中,入射角为-5.3°,0°,5.3°,7.5°,10°,入口马赫数为0.4,Tu为1.5%。用微型5孔压力探头在凹坑的叶片上进行总压力损失系数和叶片负载力的测量,并将其与光滑叶片进行比较。实验结果表明,在入射角为0°,5.3°和7.5°时,凹痕叶片的总压力损失系数的降低是明显的,而凹痕叶片的总压力损失系数的变化在入射角为0时很小。入射角为-5.3°和10°。另外,带有凹坑的叶片的加载力略有增加。比较结果还表明,在所有入射角下,吸入侧30%-60%的凹痕比吸入侧75%-95%的凹痕更有效。

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