Title of article :
An experimental and modeling study of surrogate mixtures of n-propyl- and n-butylbenzene in n-heptane to simulate n-decylbenzene ignition
Author/Authors :
Darcy، نويسنده , , Daniel and Nakamura، نويسنده , , Hisashi and Tobin، نويسنده , , Colin J. and Mehl، نويسنده , , Marco and Metcalfe، نويسنده , , Wayne K. and Pitz، نويسنده , , William J. and Westbrook، نويسنده , , Charles K. and Curran، نويسنده , , Henry J.، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2014
Pages :
14
From page :
1460
To page :
1473
Abstract :
This paper presents experimental data for the oxidation of two surrogates for the large alkylbenzene class of compounds contained in diesel fuels, namely n-decylbenzene. A 57:43 molar% mixture of n-propylbenzene:n-heptane in air (21% O 2 , 79% N 2 ) was used in addition to a 64:36 molar% mixture of n-butylbenzene:36% n-heptane in air. These mixtures were designed to contain a similar carbon/hydrogen ratio, molecular weight and aromatic/alkane ratio when compared to n-decylbenzene. Nominal equivalence ratios of 0.3, 0.5, 1.0 and 2.0 were used. Ignition times were measured at 1 atm in the shock tube and at pressures of 10, 30 and 50 atm in both the shock tube and in the rapid compression machine. The temperature range studied was from approximately 650–1700 K. The effects of reflected shock pressure and equivalence ratio on ignition delay time were determined and common trends highlighted. It was noted that both mixtures showed similar reactivity throughout the temperature range studied. A reaction mechanism published previously was used to simulate this data. Overall the reaction mechanism captures the experimental data reasonably successfully with a variation of approximately a factor of 2 for mixtures at 10 atm and fuel-rich and stoichiometric conditions.
Keywords :
Ignition , Shock tube , Rapid compression machine , n-Propylbenzene , Heptane , n-Butylbenzene
Journal title :
Combustion and Flame
Serial Year :
2014
Journal title :
Combustion and Flame
Record number :
2277436
Link To Document :
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