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Scanned-Wavelength-Modulation Spectroscopy in the Mid-Infrared for Measurements of Temperature and CO in Aluminized Composite-Propellant Flames

机译:中红外扫描波长调制光谱法,用于测量镀铝复合推进剂火焰中的温度和CO

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This work presents the application of a scanned-wavelength-modulation spectroscopy diagnostic for measuring the bulk gas temperature and CO concentration in flames of aluminized composite propellants of ammonium perchlorate (AP) and hydroxyl-terminated polybutadi-ene (HTPB). The temperature of two propellant flames (one with and one without aluminum) was measured at atmospheric pressure and various heights above the propellant surface. The maximum quasi-steady flame temperatures were 2544 and 2389 K for the propellants with and without aluminum, respectively. The temperature measured closest to the propellant surface (0.2 cm above the surface) was more than 150 K lower in the aluminized-propellant flame due to the delayed ignition of the aluminum particles. Measurements of path-integrated CO mole fraction indicate that air entrainment has a significant impact on the thermochemical structure of these flames. The results presented are the first to quantify how the bulk gas temperature of an aluminized composite-propellant flame varies with the distance above the burning surface.
机译:这项工作提出了一种扫描波长调制光谱诊断技术在测量高氯酸铵(AP)和羟基封端的聚丁二烯(HTPB)的铝化复合推进剂火焰中的总气体温度和一氧化碳浓度中的应用。在大气压下和在推进剂表面上方的不同高度下,测量了两种推进剂火焰的温度(一种带有铝,一种没有铝)。含铝和不含铝的推进剂的最大准稳态火焰温度分别为2544和2389K。在铝化推进剂火焰中,由于铝颗粒的延迟点火,最接近推进剂表面(在表面上方0.2 cm)处测得的温度降低了150 K以上。路径积分CO摩尔分数的测量结果表明,夹带空气对这些火焰的热化学结构具有重大影响。给出的结果是第一个量化镀铝复合推进剂火焰的总体气体温度如何随燃烧表面上方距离变化的方法。

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