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IGNITION AND COMBUSTION OF PYROTECHNICS AT LOW PRESSURES AND AT TEMPERATURE EXTREMES

机译:低压和高温下烟火技术的点火和燃烧

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Rapid and effective ignition of pyrotechnic countermeasure decoy flares is vitallyimportant to the safety of expensive military platforms such as aircraft. QinetiQ isconducting experimental and theoretical research into pyrotechnic countermeasuredecoy flares. A key part of this work is the development and application ofimproved models to increase the understanding of the ignition processes occurringfor these flares. These models have been implemented in a two-dimensionalcomputational model and details are described in this paper. Previous work hasconducted experiments and validated the computational model at ambienttemperature and pressure. More recently the computational model has beenvalidated at pressures down to that equivalent to 40,000 feet but at ambienttemperature (~290K). This paper describes further experimental work in which theignition delays of the priming material in inert countermeasure decoy flares weredetermined for pressures down to 40,000 feet and at temperature extremes of -40°C and 100°C. Also included in this paper is a comparison of the measured andpredicted ignition delays at low pressures and temperature extremes. Theagreement between the predicted and measured ignition delays is acceptable. Thispaper is an extended abstract – the full paper appears in Defence Technology,Volume 13, Number 3.
机译:快速有效地点燃烟火对策诱饵火炬至关重要 对于昂贵的军事平台(例如飞机)的安全至关重要。 QinetiQ是 对烟火对策进行实验和理论研究 诱饵弹。这项工作的关键部分是开发和应用 改进了模型,以加深对点火过程的了解 这些耀斑。这些模型已在二维中实现 本文介绍了计算模型和详细信息。以前的工作有 进行实验并验证环境下的计算模型 温度和压力。最近,计算模型已经 在低至40,000英尺的压力下但在环境压力下进行了验证 温度(〜290K)。本文介绍了进一步的实验工作,其中 惰性对策诱饵火炬中引爆材料的点火延迟为 确定用于低至40,000英尺的压力和极端温度- 40°C和100°C。本文还包括对实测值和实测值的比较。 在低压和极端温度下的预计点火延迟。这 预测的点火延迟和测量的点火延迟之间的一致性是可以接受的。这 论文是扩展的摘要–全文发表在《国防技术》中, 第13卷,第3期。

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