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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University of Belgrade - Faculty of Mechanical Engineering, Belgrade
2018-01-01
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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 |
work_keys_str_mv |
AT anetorlucky simulationstudiesofcombustioninaconstantmassvariablevolumecombustionchamber AT osakueedwarde simulationstudiesofcombustioninaconstantmassvariablevolumecombustionchamber |
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