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Novel optical heating rate measurement in hypersonic flow using phenol formaldehyde luminescence

机译:使用苯酚甲醛发光的高超声速中的新型光学加热速率测量

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A phenyl formaldehyde resin sphere model is created and subjected to Mach 7 flow. The model produces temperature-dependent luminescence without chemical modification or doping with a luminescent probe. The luminescent images are captured at a rate of 20Hz during a total testing time of 5.5s. The luminescent images are used to non-intrusively calculate spatially and temporally resolved maps of the temperature over the surface of the model. From this, the heating rate at various locations along the sphere model is calculated. This heating rate is compared to an analytical model for hypersonic flow over a hemisphere. (C) 2021 Elsevier Masson SAS. All rights reserved.
机译:产生苯基甲醛树脂球模型并进行马赫7流。 该模型产生温度依赖性发光,而无需化学改性或用发光探针掺杂。 在总测试时间为5.5s的情况下,在20Hz的速率下捕获发光图像。 发光图像用于非侵入性地计算模型表面上的温度的空间和时间分辨地图。 由此,计算沿着球模型的各个位置处的加热速率。 将这种加热速率与半球上的过度流动的分析模型进行比较。 (c)2021 Elsevier Masson SAS。 版权所有。

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