首页> 外文会议>International Annual Conference of ICT >INFLUENCE OF THE INJECTOR INLET ANGLE ON THE FLOW AND SPRAY BEHAVIOUR OF SHEAR THINNING FLUIDS IN IMPINGING JET INJECTORS
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INFLUENCE OF THE INJECTOR INLET ANGLE ON THE FLOW AND SPRAY BEHAVIOUR OF SHEAR THINNING FLUIDS IN IMPINGING JET INJECTORS

机译:喷射器入口角对撞击喷射器喷射器中剪切稀化流体的流动和喷射行为的影响

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A new experimental setup has been assembled to characterize the flow and breakup behaviour of gelled propellants under impinging jet conditions for different injector inlet angles. Pressure losses as well as shadowgraph images from two perpendicular directions have been recorded for that investigation. The pressure loss measurements showed that in the laminar flow regime, where generalized Reynolds numbers are lower than approximately 2300, the influence of the injector inlet angle is negligible. In the turbulent flow regime for generalized Reynolds numbers higher than approximately 2300, a distinct influence of the inlet angle is visible. Shadowgraph images delivered a complete spacial observation of the spray. The variation of the interior inlet angle of the impinging jet injector has less influence to the breakup characteristic of the investigated fluids than the correlation to the Reynolds number. For the presented experiments in the laminar flow region, where low generalized Reynolds numbers occur, a fluid sheet is formed at the impinging point, which decays into ligaments and finally into droplets. For the presented experiments in the turbulent region the ligament pattern is found for medium generalized Reynolds numbers and the fully developed spray regime with an immediate breakup into droplets occurs for high generalized Reynolds numbers.
机译:已经组装了一种新的实验装置,以表征凝胶推进剂在撞击的喷射条件下的流动和分散行为,用于不同的喷射器入口角度。对该调查记录了压力损失以及来自两个垂直方向的影子图像图像。压力损失测量表明,在流动状态下,其中广义雷诺数低于约2300,喷射器入口角的影响可忽略不计。在高于约2300的广义雷诺数的湍流状态中,入口角度的不同影响是可见的。影子图图像送出了喷雾的完全间隔观察。撞击喷射器的内部入口角的变化对研究流体的分解特性的影响较小,而不是与雷诺数的相关性。对于层流区域中的呈现实验,其中发生低一般化的雷诺数,在撞击点处形成流体片,该撞击点拧入韧带并最终进入液滴。对于湍流区域中的呈现实验,发现韧带图案用于介质广义雷诺数,并且在高通用的雷诺数的情况下发生具有立即分解的完全发育的喷射制度。

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