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d(2) Law and Penetration Length of Jatropha and Camelina Bio-Synthetic Paraffinic Kerosene Spray Characteristics at Take-Off, Top of Climb and Cruise

机译:d(2) 麻疯树和亚麻荠生物合成石蜡煤油喷雾在起飞、爬升和巡航时的规律和穿透长度

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摘要

A comparison of d(2) law and penetration length of biofuels with Jet-A through the incorporation of fuel properties and actual combustor inlet data at various flight trajectories is presented. This study aims to identify fuel properties and flight operating conditions that most influence droplet characteristics accurately. The study comprises two phases involving a simulation using GSP to predict combustor inlet data for the respective flight operating conditions and a simulation using ANSYS Fluent V18.1 to obtain combustion characteristics of biofuels and Jet-A. The biofuels chosen in this study are Jatropha Bio-synthetic Paraffinic Kerosene (JSPK) and Camelina Bio-synthetic Paraffinic Kerosene (CSPK), evaluated as pure (100) and blend (50) with Jet-A. Thrust specific fuel consumption (TSFC) of biofuels is improved due to lower fuel consumed by the engine. The d(2) law curve shows a heat-up period that takes place at the early stage of the combustion process. The penetration length of the fuels is shorter at take-off. Combusting biofuels reduce combustion temperature and the penetration length of the droplet.
机译:通过结合燃料特性和不同飞行轨迹下的实际燃烧室入口数据,比较了生物燃料与Jet-A的d(2)定律和穿透长度。本研究旨在准确确定最能准确影响液滴特性的燃料特性和飞行操作条件。该研究包括两个阶段,包括使用GSP预测相应飞行运行条件的燃烧室入口数据的仿真,以及使用ANSYS Fluent V18.1获得生物燃料和Jet-A的燃烧特性的仿真。本研究中选择的生物燃料是麻疯树生物合成石蜡煤油 (JSPK) 和亚麻荠生物合成石蜡煤油 (CSPK),评估为纯 (100%) 和与 Jet-A 混合 (50%)。由于发动机消耗的燃料较低,生物燃料的推力比燃料消耗(TSFC)得到改善。d(2) 定律曲线显示了在燃烧过程的早期阶段发生的加热期。燃料的穿透长度在起飞时较短。燃烧生物燃料可降低燃烧温度和液滴的穿透长度。

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