کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
6630907 | 1424938 | 2018 | 7 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
A shock tube study of jet fuel pyrolysis and ignition at elevated pressures and temperatures
ترجمه فارسی عنوان
مطالعه لوله شوک جت پیلوریلیز و احتراق در فشار و درجه حرارت بالا
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کلمات کلیدی
سوخت موشک، لوله شوک، جذب لیزر، مشخصه سوخت، مدلهای ترکیبی
موضوعات مرتبط
مهندسی و علوم پایه
مهندسی شیمی
مهندسی شیمی (عمومی)
چکیده انگلیسی
The development of compact HyChem hybrid models for jet fuels requires datasets of pyrolysis product yields to constrain the model and of kinetic targets to evaluate the model. To this end, we have measured selected species time-histories during fuel pyrolysis using laser absorption, and ignition delay times using multiple methods behind reflected shock waves in a heated shock tube. Measurements were performed for three different jet fuels diluted in air or argon over a temperature range of 1000-1400â¯K, a pressure range of 12-40â¯atm, and equivalence ratios of 0.5-1. Fuel loading was measured using an IR He-Ne laser at 3391â¯nm; ethylene with a CO2 gas laser at wavelengths of 10532â¯nm and 10674â¯nm; and methane with a tunable diode laser at wavelengths of 3175â¯nm and 3177â¯nm. Ignition delay times were measured in three ways: by monitoring fuel removal with laser absorption, by sidewall pressure, and by OHâ emission. Particular care was taken in mixture preparation and efficient transfer of the gaseous fuel mixture to the shock tube. The current HyChem model by Wang et al. shows good agreement with these data.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Fuel - Volume 226, 15 August 2018, Pages 338-344
Journal: Fuel - Volume 226, 15 August 2018, Pages 338-344
نویسندگان
Jiankun Shao, Yangye Zhu, Shengkai Wang, David F. Davidson, Ronald K. Hanson,