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NUMERICAL CALIBRATION AND INVESTIGATION OF THE INFLUENCE OF REYNOLDS NUMBER ON MEASUREMENTS WITH FIVE-HOLE PROBES IN COMPRESSIBLE FLOWS

机译:雷诺数对压缩流动五孔探头测量雷诺数对雷诺数的数值校准及调查

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This paper presents an investigation into the numerical and experimental calibration of a five-hole probe and effects of Reynolds number variations on the characteristics of the probe. The test object is a cone-type drilled elbow probe with a head diameter of 1.59 mm and a cone angle of 60°. The experimental calibration maps of four different probes of the same type and nominal geometry are compared. A significant variation of the curves can be observed especially at high yaw angles. This led to a visual inspection of the probes with a 3D measurement system. The actual geometry of the three used probes and the surface and radii in particular varied significantly from that of the unused spare probe. Furthermore, a numerical calibration map of the ideal probe was generated for a Much number of Ma = 0.3. A comparison between the experimental and numerical calibration coefficients revealed that total pressure, yaw and pitch angle were reproduced reasonably well. The dynamic pressure coefficient, however, has a considerable offset. Finally, a parameter study of the effect of varying the Reynolds number over different yaw angles was conducted. The calibration Reynolds number is of the order of Re = 1 · 10~4 and was varied between 0.5 · 10~4 < Re < 6 · 10~4. While the results suggest that only minor measurement errors occur for yaw angle, total pressure and static pressure, a relatively large error was observed for pitch angle measurements.
机译:本文提出了对五孔探头的数值和实验校准的调查,以及雷诺数变异对探针特性的影响。测试对象是锥形钻孔弯头探针,头径为1.59毫米,锥角为60°。比较了相同类型和标称几何形状的四种不同探针的实验校准映射。曲线的显着变化可以特别地观察到高偏航角度。这导致了具有3D测量系统的探头的目视检查。三种使用的探针和表面和半径的实际几何形状特别是未使用的备用探针的显着变化。此外,为许多MA = 0.3产生了理想探针的数值校准图。实验和数值校准系数之间的比较揭示了总压力,横摆和俯仰角度的相当良好地再现。然而,动态压力系数具有相当大的偏移。最后,进行了改变不同偏航角度改变雷诺数的效果的参数研究。校准雷诺数是Re = 1·10〜4的顺序,在0.5·10〜4

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