首页> 外文会议>31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit July 10-12, 1995/San Diego, CA >Modeling and experiments of laser-induced ignition of nitramine propellants
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Modeling and experiments of laser-induced ignition of nitramine propellants

机译:激光诱导硝胺推进剂点火的建模与实验

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The objective of the work is to develop and experimentally verify a model for CO_2 laser-induced ignition of nitramine-based propellants. The one-dimensional model considers heat conduction in the condensed phase coupled to heat and mass transport with global chemical kinetics of a heterogeneous propellant in the gas-phase region. The highly nonlinear model was solved numerically. Experimentally, increases in heat flux (125 - 375 W/cm~2) lowered the ignition delay time but changes in pressure the assumption that RDX decomposition is primarily temperature controlled. These trends are correctly predicted by the model. Predictions of ignition delay time fall within the experimental uncertainty. Sensitivities of the numerical solution to the material properties and kinetic rate constants are addressed.
机译:这项工作的目的是开发和实验验证CO_2激光诱导的硝胺基推进剂点火模型。一维模型考虑了凝结相中的热传导与热和质量传递,以及气相区域中异质推进剂的整体化学动力学。对高度非线性的模型进行了数值求解。在实验上,热通量的增加(125-375 W / cm〜2)减少了点火延迟时间,但在压力变化的前提下假设RDX分解主要是受温度控制的。这些趋势已由模型正确预测。点火延迟时间的预测落在实验不确定性范围内。解决了对材料特性和动力学速率常数的数值解的敏感性。

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