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A Fluid Flow Analysis of the Gaseous Impact Test

机译:气体冲击试验的流体流动分析

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The Gaseous Impact Test is simulated using fluid dynamics numerical models. Pressure overshoots observed at Centre de Technologies et d'Expertises are matched by one-dimensional computations. Peak temperatures are evaluated when including irreversible processes. Formation of a temperature gradient within the hot gas plug has been identified and an explanation is provided. The influence of geometrical design parameters is studied. Temperature history requires use of a two-dimensional model for it enables description of vortex-induced mixing as a consequence of the reflected shock bifurcation at the test tube end. A cellular structure is formed in the pressure field. Skin temperature of different wall materials has also been evaluated. Short versus long test tube effects are discussed.
机译:使用流体动力学数值模型进行模拟气态冲击试验。在Center de Technologies et d'专业中观察到的压力过冲与一维计算匹配。在包括不可逆过程时评估峰值温度。已经鉴定了热气塞内的温度梯度的形成,并提供了解释。研究了几何设计参数的影响。温度历史需要使用二维模型,其能够描述涡旋诱导的混合作为试管端的反射冲击分叉的结果。在压力场中形成蜂窝结构。还评估了不同壁材料的皮肤温度。讨论了短暂的测试管效应。

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