首页> 外文会议>International symposium on air breathing engines;ISABE 2011 >INVESTIGATIONS OF A COMBUSTOR USING A 9-POEVT SWIRL-VENTURI FUEL INJECTOR: RECENT EXPERIMENTAL RESULTS
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INVESTIGATIONS OF A COMBUSTOR USING A 9-POEVT SWIRL-VENTURI FUEL INJECTOR: RECENT EXPERIMENTAL RESULTS

机译:使用9角涡流文丘里燃料喷射器对燃烧室进行的研究:最近的实验结果

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This paper explores recent results obtained during testing in an optically-accessible, JP8-fueled, flame tube combustor using baseline lean direct injection (LDI) research hardware. The baseline LDI geometry has 9 fuel/air mixers arranged in a 3 x 3 array. Results from this 9-element array include images of fuel and OH speciation via planar laser-induced fluorescence (PLIF), which describe fuel spray pattern and reaction zones. Preliminary combustion temperatures derived from Stokes/Anti-Stokes Spontaneous Raman Spectroscopy are also presented. Other results using chemiluminescence from major combustion radicals such as CH~* and C_2~* serve to identify the primary reaction zone, while OH PLIF shows the extent of reaction further downstream. Air and fuel velocities and fuel drop size results are also reported.
机译:本文探讨了使用基线稀薄直接喷射(LDI)研究硬件在以光学方式访问,使用JP8燃料的火焰管燃烧器中进行测试期间获得的最新结果。基准LDI几何结构具有9个以3 x 3阵列排列的燃油/空气混合器。这个由9个元素组成的阵列的结果包括通过平面激光诱导的荧光(PLIF)生成的燃料和OH形态的图像,这些图像描述了燃料的喷射方式和反应区。还介绍了从斯托克斯/反斯托克斯自发拉曼光谱学得出的初步燃烧温度。使用来自主要燃烧自由基(例如CH〜*和C_2〜*)的化学发光的其他结果可用于识别主要反应区,而OH PLIF显示出更下游的反应程度。还报告了空气和燃料的速度以及燃料滴的大小。

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