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Numerical investigations of flow characteristics of a pumpjet propulsor in oblique inflow

机译:斜流入泵喷头推进器流动特性的数值研究

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In this study, a detailed analysis of hydrodynamic performance of a pumpjet propulsor (PJP) in different oblique inflow angles (beta = 0 degrees , 5 degrees , 10 degrees , 15 degrees , 20 degrees, 25 degrees, 30 degrees, 40 degrees) and different rotational speeds (n= 3000rpm, 3600rpm, 4200rpm) is investigated numerically. The SST k-omega turbulence model and sliding mesh technology based on the Reynolds Averaged Navier-Stokes (RANS) method are employed. The structured grids are adopted to the whole computational domain. The grid independent inspection is carried out and verified. A ducted propeller (the Ka470 propeller in 19A duct) is selected to validate the numerical method by comparison of its results with experimental data. Based on the numerical method, it can be found that the propulsor efficiency decreased with the increasing of different beta. The propulsor efficiency changes tinily in little oblique angle and decreases significantly when the oblique angle is larger than 20 degrees. The thrust coefficient and torque coefficient of PJP are obtained. The increase of beta has a negative impact on the balance performance of PJP. The pressure distributions of pressure and suction side of rotor blade with different beta are analyzed. Owing to the influence of beta, the pressure of the upper left region of rotor blade drops significantly. The enlargement of the local load on pressure side and the appearance and expansion of the low-pressure region on suction side occour at the bottom right region of rotor blade. The radial distributions of the axial velocity (V-z) and the tangential velocity (V-t) with different Span and beta along the axial direction are investigated. The increase of beta resultes in a severe oscillatory behavior of the flow velocity, which easily induces the occurrence of cavitation phenomenon and mechanical vibration. The velocity contours of the axial cross section with different beta are presented. Due to the change of beta, the flows are blocked by the flow-guide and duct, there are obvious high-velocity and low-velocity regions of the flows.
机译:在这项研究中,详细分析了泵喷头推进器(PJP)的不同倾斜流入角(β= 0度,5度,10度,15度,20度,25度,30度,40度)和在数值上对不同的转速(n = 3000rpm,3600rpm,4200rpm)进行了调查。基于Reynolds的SST k-Omega湍流模型和滑动网格技术采用了reynolds vier-stokes(RANS)方法。结构化网格被采用到整个计算领域。进行网格独立检验并验证。通过将其结果与实验数据进行比较,选择管道螺旋桨(19A管道中的KA470螺旋桨)以验证数值方法。基于数值方法,可以发现推进效率随着不同β的增加而降低。推进效率几乎倾斜地变化,并且当倾斜角度大于20度时,显着减小。获得PJP的推力系数和扭矩系数。 Beta的增加对PJP的平衡表现产生负面影响。分析了具有不同β的转子叶片的压力和吸力侧的压力分布。由于β的影响,转子叶片的左上区域的压力显着下降。在转子叶片底部右区域的吸入侧面侧的压力侧的局部负荷和低压区域的外观和膨胀的放大。研究了轴向速度(V-Z)的径向分布和沿着轴向的不同跨度和β的切向速度(V-T)。 β的增加导致了流速的严重振荡行为,这很容易诱导空化现象和机械振动的发生。提出了具有不同β的轴向横截面的速度轮廓。由于β的变化,流动由流动引导和管道阻挡,流动的高速度和低速区域。

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