Simulation studies of combustion in a constant-mass variable-volume combustion chamber

A numerical simulation code was used to conduct a systematic study of the effects of fuel-air equivalence ratios in the range 0.7 ≤ φ ≤ 1.4 and compression ratio, rc = 8.0 on key operating parameters, such as pressure, rate of change of pressure, '/dt' flame extinction temperature, burn ra...

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Main Authors: Anetor Lucky, Osakue Edward E.
Format: Article
Language:English
Published: University of Belgrade - Faculty of Mechanical Engineering, Belgrade 2018-01-01
Series:FME Transactions
Subjects:
Online Access:https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2018/1451-20921804475A.pdf
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spelling doaj-be5e16669c35471db01b629fedc79e8d2020-11-25T03:10:35ZengUniversity of Belgrade - Faculty of Mechanical Engineering, BelgradeFME Transactions1451-20922406-128X2018-01-014644754881451-20921804475ASimulation studies of combustion in a constant-mass variable-volume combustion chamberAnetor Lucky0Osakue Edward E.1Nigerian Defence Academy, Department of Mechanical Engineering, Kaduna, NigeriaTexas Southern University, Department of Industrial Technologies, Houston, Texas, USAA numerical simulation code was used to conduct a systematic study of the effects of fuel-air equivalence ratios in the range 0.7 ≤ φ ≤ 1.4 and compression ratio, rc = 8.0 on key operating parameters, such as pressure, rate of change of pressure, '/dt' flame extinction temperature, burn rate frequency, combustion efficiency, ηb, source term, mass burn fractions and heat loss in a simulated 5.734 liter, V8 spark-ignition engine. The data shows that the burn rate characteristics of the fuel and oxidizer are qualitatively perfectly correlated. The results also show that as flame extinction/flameout is approached, the fuel consumption rate, Rfu increases rapidly with temperature for fuel-air equivalence ratios, φ in the range 0.7 ≤ φ ≤ 1.4. The average burn rate frequency (per second), fbr(1/s) varies from 11.2 ≤ fbr ≤ 137.0 for fuel-air equivalence ratios, φ in the range 0.7 ≤ φ ≤ 1.4 The results further show that the fastest fuel consumption rate was for fuel-air equivalence ratio, φ = 1.4 in the time interval, t such that 0.0 ≤ t ≤ 0.61 ms while the slowest corresponds to φ - 0.7 and the corresponding time interval was 0.0 ≤ t ≤ 3.98 ms. Moreover, the data shows that for fuel-air equivalence ratios, φ in the range 0.7 ≤ φ ≤ 1.4 the fuel consumption rate increases monotonically after the initial ignition delay period. The combustion efficiency, ηb of the engine under investigation were found to be in the range of 94.1% ≤ ηb ≤ 94.4% for lean mixtures, that is, for φ < 1.0;the corresponding values of combustion efficiency, ηb for fuel-rich mixtures were in the interval 93.8% ≤ ηb ≤ 94.1%. The other results from this study are summarized in the conclusion.https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2018/1451-20921804475A.pdffuel-air equivalence ratiocompression ratioextinction flame temperatureburn rate frequencycombustion efficiencyengine knockactivation energy
collection DOAJ
language English
format Article
sources DOAJ
author Anetor Lucky
Osakue Edward E.
spellingShingle Anetor Lucky
Osakue Edward E.
Simulation studies of combustion in a constant-mass variable-volume combustion chamber
FME Transactions
fuel-air equivalence ratio
compression ratio
extinction flame temperature
burn rate frequency
combustion efficiency
engine knock
activation energy
author_facet Anetor Lucky
Osakue Edward E.
author_sort Anetor Lucky
title Simulation studies of combustion in a constant-mass variable-volume combustion chamber
title_short Simulation studies of combustion in a constant-mass variable-volume combustion chamber
title_full Simulation studies of combustion in a constant-mass variable-volume combustion chamber
title_fullStr Simulation studies of combustion in a constant-mass variable-volume combustion chamber
title_full_unstemmed Simulation studies of combustion in a constant-mass variable-volume combustion chamber
title_sort simulation studies of combustion in a constant-mass variable-volume combustion chamber
publisher University of Belgrade - Faculty of Mechanical Engineering, Belgrade
series FME Transactions
issn 1451-2092
2406-128X
publishDate 2018-01-01
description A numerical simulation code was used to conduct a systematic study of the effects of fuel-air equivalence ratios in the range 0.7 ≤ φ ≤ 1.4 and compression ratio, rc = 8.0 on key operating parameters, such as pressure, rate of change of pressure, '/dt' flame extinction temperature, burn rate frequency, combustion efficiency, ηb, source term, mass burn fractions and heat loss in a simulated 5.734 liter, V8 spark-ignition engine. The data shows that the burn rate characteristics of the fuel and oxidizer are qualitatively perfectly correlated. The results also show that as flame extinction/flameout is approached, the fuel consumption rate, Rfu increases rapidly with temperature for fuel-air equivalence ratios, φ in the range 0.7 ≤ φ ≤ 1.4. The average burn rate frequency (per second), fbr(1/s) varies from 11.2 ≤ fbr ≤ 137.0 for fuel-air equivalence ratios, φ in the range 0.7 ≤ φ ≤ 1.4 The results further show that the fastest fuel consumption rate was for fuel-air equivalence ratio, φ = 1.4 in the time interval, t such that 0.0 ≤ t ≤ 0.61 ms while the slowest corresponds to φ - 0.7 and the corresponding time interval was 0.0 ≤ t ≤ 3.98 ms. Moreover, the data shows that for fuel-air equivalence ratios, φ in the range 0.7 ≤ φ ≤ 1.4 the fuel consumption rate increases monotonically after the initial ignition delay period. The combustion efficiency, ηb of the engine under investigation were found to be in the range of 94.1% ≤ ηb ≤ 94.4% for lean mixtures, that is, for φ < 1.0;the corresponding values of combustion efficiency, ηb for fuel-rich mixtures were in the interval 93.8% ≤ ηb ≤ 94.1%. The other results from this study are summarized in the conclusion.
topic fuel-air equivalence ratio
compression ratio
extinction flame temperature
burn rate frequency
combustion efficiency
engine knock
activation energy
url https://scindeks-clanci.ceon.rs/data/pdf/1451-2092/2018/1451-20921804475A.pdf
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