Plume centerline temperature 羽流中心温升
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The plume temperature is an important parameter, for solid propellant rocket engines and it is useful for determining the combustion process of the engine.
推进剂的羽焰温度是固体推进剂火箭发动机的重要参数，对于研究发动机内的燃烧过程具有重要价值。
The application of remote sensing FTIR spectrometry in determination of the absolute radiation energy, combustion gas concentration and propellant plume temperature was reviewed.
介绍了遥感傅立叶变换红外光谱测试技术的优点，综述了遥感FTIR光谱技术在固体推进剂羽焰红外绝对辐射能量、羽焰温度、燃气浓度测定中的应用。
The results indicated that the shape of steam plume was influenced by the inlet steam pressure and subcooled water temperature.
结果表明入口蒸汽压力和过冷水温度是影响汽羽形状的主要因素。
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