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The effect of Reynolds number on the propulsive efficiency of a biomorphic pulsed-jet underwater vehicle

机译:雷诺数对生物形态脉冲喷射水下航行器推进效率的影响

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The effect of Reynolds number on the propulsive efficiency of pulsed-jet propulsion was studied experimentally on a self-propelled, pulsed-jet underwater vehicle, dubbed Robosquid due to the similarity of its propulsion system with squid. Robosquid was tested for jet slug length-to-diameter ratios (L/D) in the range 2-6 and dimensionless frequency (St_L) in the range 0.2-0.6 in a glycerin-water mixture. Digital particle image velocimetry was used for measuring the impulse and energy of jet pulses from the velocity and vorticity fields of the jet flow to calculate the pulsed-jet propulsive efficiency, and compare it with an equivalent steady jet system. Robosquid's Reynolds number (Re) based on average vehicle velocity and vehicle diameter ranged between 37 and 60. The current results for propulsive efficiency were compared to the previously published results in water where Re ranged between 1300 and 2700. The results showed that the average propulsive efficiency decreased by 26% as the average Re decreased from 2000 to 50 while the ratio of pulsed-jet to steady jet efficiency (η_P/η_(P, ss)) increased up to 0.15 (26%) as the Re decreased over the same range and for similar pulsing conditions. The improved η_P/η_(P, ss) at lower Re suggests that pulsed-jet propulsion can be used as an efficient propulsion system for millimeter-scale propulsion applications. The Re = 37-60 conditions in the present investigation, showed a reduced dependence of η_P and η_P/η_(P, ss)on L/D compared to higher Re results. This may be due to the lack of clearly observed vortex ring pinch-off as L/D increased for this Re regime.
机译:由于其推进系统与鱿鱼的相似性,在被称为Robosquid的自推进式脉冲喷射水下航行器上,实验研究了雷诺数对脉冲喷射推进力的影响。测试了Robosquid在甘油-水混合物中的射流塞长径比(L / D)在2-6范围内,无量纲频率(St_L)在0.2-0.6范围内。使用数字粒子图像测速仪从射流的速度场和旋涡场测量射流脉冲的脉冲和能量,以计算脉冲射流推进效率,并将其与等效的稳定射流系统进行比较。根据平均车速和车辆直径,Robosquid的雷诺数(Re)在37至60之间。将当前推进效率的结果与先前公布的Re在1300至2700之间的水中的结果进行了比较。结果表明,平均推进力当平均Re从2000降低到50时,效率降低了26%,而随着Re的降低,脉冲射流与稳定射流效率之比(η_P/η_(P,ss))增加到0.15(26%)范围和类似的脉冲条件。较低Re时改进的η_P/η_(P,ss)表明,脉冲射流推进可以用作毫米级推进应用的有效推进系统。在本研究中,Re = 37-60的条件表明,与较高的Re结果相比,η_P和η_P/η_(P,ss)对L / D的依赖性降低。这可能是由于在此Re方案中,随着L / D的增加,缺乏清晰观察到的涡环夹断。

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