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Upward Propagation of Very Lean Methane-Air Flames in Vertical Tubes

机译:竖管中极贫甲烷空气火焰的向上传播

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The upward propagation of a lean methane-air flame front in a vertical tube is investigated. The velocity of the flame front has been measured with an array of photodiodes set along the tube wall and, independently, from photographic records. A PIV system triggered by a photodiode signal has been used to measure the velocity of the flow induced by the flame front in a vertical plane through the axis of the tube. The contour of the luminous region of the flame front, assumed cylindrically symmetric, has been extracted from the recorded images. As expected, the shape and velocity of a very lean flame front, and the velocity of the fresh gas relative to the front, are similar to those of a bubble rising in the tube. The flow of the burnt gas features a region of low velocity (relative to the flame front) which enhances radiation losses and seems to play an important role in the extinction of the flame at the flammability limit. This limit is found to depend very sensitively on the temperature of the tube wall. A simple model is proposed of the flow around the axis of the tube and the combustion around the tip of the flame front. This model uses the measured gas velocity at the axis of the tube together with simplified conservation equations to compute the temperature and species concentrations along the axis for a given kinetic scheme and radiation law. The results for a single overall Arrhenius reaction and for a four-step reduced scheme, both in an optically thin gas, are in reasonable agreement with our experimental data and shed some light on the roles played by radiation losses and kinetic effects on the flammability limit measured in the standard flammability tube. The model can also be used to test other kinetic schemes and radiation laws.
机译:研究了在垂直管中稀薄的甲烷-空气火焰前沿的向上传播。火焰前沿的速度已通过沿管壁设置的光电二极管阵列进行测量,并且独立于摄影记录。由光电二极管信号触发的PIV系统已被用于测量由火焰前沿在垂直于管轴的平面内引起的流动速度。从记录的图像中提取出假定为圆柱对称的火焰前部发光区域的轮廓。不出所料,非常稀薄的火焰前沿的形状和速度以及新鲜气体相对于前沿的速度类似于气泡在管中上升的速度。燃烧气体的流动具有一个低速区域(相对于火焰前沿),该区域会增加辐射损失,并且似乎在可燃性极限处的火焰熄灭中起着重要作用。发现该极限非常敏感地取决于管壁的温度。提出了一个简单的模型,该模型是围绕管子轴线的流动和围绕火焰前沿的燃烧。该模型使用在管轴处测得的气体速度以及简化的守恒方程来针对给定的动力学方案和辐射定律计算沿轴的温度和物质浓度。在光学上稀薄的气体中,单一的整体Arrhenius反应和四步还原方案的结果与我们的实验数据合理地吻合,并阐明了辐射损失和动力学对可燃性极限所起的作用在标准易燃管中测量。该模型还可以用于测试其他动力学方案和辐射定律。

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