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Experimental Shock Tube Measurements of Laminar Burning Velocity of n-Heptane and iso-Octane in the Negative Temperature Coefficient Regime

机译:在负温度系数制度中正庚烷和异辛烷的层状燃烧速度的实验冲击管测量

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Laminar burning velocities (S_L) of n-heptane and iso-octane are measured between 400 and 900 K at 1 atm and 0.9 equivalence ratio. A shock tube is used to heat the unburned gas to temperatures at which it would auto-ignite, while limiting the time for ignition chemistry to occur ahead of the flame to much less than the ignition delay time. In air (21% O_2, 79% N_2), measured values of S_l are lower than, but follow the same temperature trend as the model below 550 K; between 550 and 600 K, a stronger dependence of S_L on temperature is observed. For S_l measurements performed in a helium-containing oxidizer (18% O_2, 41% N_2, 41% He), a strong temperature dependence, similar to that seen in air, is observed between 600 and 700 K. Between 700 and 800 K, a negative temperature dependence is observed. Above 800 K, measured S_L again assumes a positive temperature dependence. While negative temperature coefficient (NTC) behavior is known to exist in ignition delay times for many hydrocarbon fuels, to the authors' knowledge, this work represents the first direct, experimental observation of NTC behavior in flame speed measurements.
机译:正庚烷和异辛烷的层流燃烧速度(S_L)的400和900处的K 1个大气压和0.9当量比之间测量的。的激波管用于将未燃气体加热到温度在其它会自动点火,同时限制时间提前的火焰的发生比点火延迟时间少得多的点火化学。在空气(21%O_2,79%N_2),S_L的测量值低于,但遵循相同的温度趋势如低于550 k中的模型; 550和600 K的,S_L对温度的依赖性更强观察。一种用于在含氦气的氧化剂进行S_L测量(18%O_2,41%N_2,41%的He),强大的温度依赖性,类似于空气看到的,600和700 K.之间观察到在700和800 K,负的温度依赖性,观察到。高于800 K,测量S_L再次取正的温度依赖性。而负温度系数(NTC)特性是已知的,点火延迟时间存在许多烃类燃料,以作者所知,这项工作表示第一直接,实验的NTC特性在火焰速度测量观察。

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