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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:负温度系数条件下正庚烷和异辛烷层流燃烧速度的实验激波管测量

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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)在1个大气压和0.9当量比的条件下在400和900 K之间测量。冲击管用于将未燃烧的气体加热到将其自动点燃的温度,同时将点燃化学物质在火焰之前发生的时间限制在比点燃延迟时间短得多的时间。在空气中(21%O_2,79%N_2),S_1的测量值低于550 K,但遵循与模型相同的温度趋势;在550和600 K之间,观察到S_L对温度的依赖性更大。对于在含氦氧化剂(18%O_2、41%N_2、41%He)中进行的S_1测量,在600至700 K之间观察到与空气中相似的强烈温度依赖性。在700至800 K之间,观察到负温度依赖性。高于800 K时,测得的S_L再次呈现正温度依赖性。尽管许多烃类燃料的点火延迟时间中都存在负温度系数(NTC)行为,但据作者所知,这项工作代表了NTC在火焰速度测量中的首次直接实验性观察。

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