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Parametric evaluation of swirl injector dynamics in the high-frequency range

机译:高频范围内旋流喷射器动力学的参数评估

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This work augments the classical linear swirl injector dynamics theory to evaluate the hydrodynamic frequency response characteristics of a single element as an analysis aid for experimental results from cold flow testing. Specific focus is placed on how surface waves within the swirl injector are modeled. A modified formulation of wave interactions within the vortex chamber includes disturbance origins displaced from the posterior wall of the injector. Differing phase delays in both downstream and upstream directions are accounted for by dispersive calculations valid at all frequencies rather than by the traditional long wave approximation. The model is semiempirically tailored to hydraulic conditions for a study element, and a response function analysis is presented for an example case. Distinct features in the range of 2000-4000 Hz are found to be predominately related to surface wave patterns within the injector's vortex chamber. Comparisons are made to experimental data, showing qualitative agreement with injector response and detection of computed high-frequency surface wave responses. Calculations are then mapped over steady mass flow conditions that range from 39 to 89% of the injector's nominal design point. The results show that response features associated with surface wave dynamics consistently manifest across the entire parameter space investigated for the study injector element.
机译:这项工作扩充了经典的线性旋流喷射器动力学理论,以评估单个元件的流体动力频率响应特性,作为对冷流测试实验结果的分析辅助。特别关注如何对旋流喷油器内的表面波建模。涡流室内的波相互作用的改进公式包括从喷射器的后壁移开的扰动源。下游方向和上游方向上不同的相位延迟是通过在所有频率下均有效的色散计算来解决的,而不是通过传统的长波近似来解决的。该模型针对研究元件的液压条件进行了半经验性的调整,并针对示例案例进行了响应函数分析。发现在2000-4000 Hz范围内的明显特征主要与喷射器涡旋室内的表面波型有关。与实验数据进行了比较,显示了与喷油器响应和计算出的高频表面波响应的定性一致性。然后将计算结果映射到稳定质量流量条件下,该稳定质量流量条件是喷油器标称设计点的39%至89%。结果表明,与表面波动力学相关的响应特征在研究的喷油器元件所研究的整个参数空间中始终表现出来。

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  • 来源
    《Journal of propulsion and power》 |2017年第5期|1218-1229|共12页
  • 作者单位

    University of Alabama in Huntsville, Huntsville, AL, United States,Department of Mechanical and Aerospace Engineering, S225 Technology Hall, United States;

    University of Alabama in Huntsville, Huntsville, AL, United States,Department of Mechanical and Aerospace Engineering, S225 Technology Hall, United States;

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