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Frontiers in Energy

ISSN 2095-1701

ISSN 2095-1698(Online)

CN 11-6017/TK

Postal Subscription Code 80-972

2018 Impact Factor: 1.701

Front. Energy    2016, Vol. 10 Issue (2) : 164-175    https://doi.org/10.1007/s11708-016-0407-9
RESEARCH ARTICLE
Assessment and validation of liquid breakup models for high-pressure dense diesel sprays
Yi REN,Xianguo LI()
Department of Mechanical and Mechatronics Engineering, University of Waterloo, Waterloo, Ontario, Canada
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Abstract

Liquid breakup in fuel spray and atomization significantly affects the consequent mixture formation, combustion behavior, and emission formation processes in a direct injection diesel engine. In this paper, different models for liquid breakup processes in high-pressure dense diesel sprays and its impact on multi-dimensional diesel engine simulation have been evaluated against experimental observations, along with the influence of the liquid breakup models and the sensitivity of model parameters on diesel sprays and diesel engine simulations. It is found that the modified Kelvin-Helmholtz (KH)–Rayleigh-Taylor (RT) breakup model gives the most reasonable predicted results in both engine simulation and high-pressure diesel spray simulation. For the standard KH-RT model, the model constant Cbl for the breakup length has a significant effect on the predictability of the model, and a fixed value of the constant Cbl cannot provide a satisfactory result for different operation conditions. The Taylor-analogy-breakup (TAB) based models and the RT model do not provide reasonable predictions for the characteristics of high-pressure sprays and simulated engine performance and emissions.

Keywords breakup model      diesel engine      high-pressure injection      simulations     
Corresponding Author(s): Xianguo LI   
Just Accepted Date: 31 March 2016   Online First Date: 17 May 2016    Issue Date: 27 May 2016
 Cite this article:   
Yi REN,Xianguo LI. Assessment and validation of liquid breakup models for high-pressure dense diesel sprays[J]. Front. Energy, 2016, 10(2): 164-175.
 URL:  
https://academic.hep.com.cn/fie/EN/10.1007/s11708-016-0407-9
https://academic.hep.com.cn/fie/EN/Y2016/V10/I2/164
Engine Caterpillar 3401E single cylinder oil test engine (SCOTE)
Bore×stroke/mm 137.2 ×165.1
Compression ratio 16.1:1
Displacement/L 2.44
Connecting rod length/mm 261.6
Squish height/mm 1.57
Intake valve closing/(°) ATDC –143
Exhaust valve opening/(°) ATDC 130
Tab.1  Engine specifications [17]
Injector type Electronic unit injector (EUI)
Maximum injection pressure/MPa 190
Number of nozzle holes 6
Nozzle hole diameter/mm 0.214
Included spray angle 130˚
Injection rate shape Rising
Tab.2  Injection system parameters [17]
Fig.1  Schematic of different liquid breakup models considered in this paper [2]

(a) KH model; (b) RT model; (c) KH-RT hybrid model

Physical process Model
Drop collision NTC model [11]
Drop turbulent dispersion O’Rourke turbulent dispersion model
Drop vaporization Amsden-Chiang model [23]
Ignition and combustion (Only used in the engine simulation) Shell+characteristic time combustion (CTC) model [24]
Pollutant formation (Only used in the engine simulation) Extended Zel’dovich model &Hiroyasu-NS coxidation soot model [25,26]
Tab.3  Other sub-models implemented in this paper
Fig.2  Grid resolutions (The experimental image is taken from Ref. [16])

(a) Corresponding simulated results; (b) sprays injected into constant-volume vessel using the KH-RT hybrid breakup model

Injection pressure/MPa Injection duration/ms Ambient temperature/K Ambient density/(kg·m–3) Injector diameter Dn/mm
180 1.0 950 60 0.1
Tab.4  Conditions for fuel sprays injected into a constant volume vessel considered in this paper
Case Breakup Model
1 KH-RT modified model
2 KH-RT model with the breakup length constant Cbl=10 in Eq. (20)
3 KH-RT model with Cbl=20 in Eq. (20)
4 KH-RT model with Cbl=40 in Eq. (20)
5 TAB model (without the drop size distribution)
6 TAB-CHI model (with the chi-squared drop size distribution)
7 TAB-RR model (with the Rosin-Rammler drop size distribution)
Tab.5  Different breakup models evaluated in this paper
Fig.3  A comparison of predicted and measured liquid spray tip penetration for fuel injected into constant-volume vessel at an ambient gas temperature of Ta = 950 K and an ambient gas density of ρa = 60 kg/ m3
Fig.4  Simulated results of vapor phase spray in constant-volume vessel at an ambient gas temperature of Ta = 950 K, an ambient gas density of ρa = 60 kg/ m3,and an injection time of 0.5 ms after the start of injection
Fig.5  Simulated results of liquid spray mass in constant-volume vessel at an ambient gas temperature of Ta = 950 K and an ambient gas density of ρa = 60 kg/ m3
Fig.6  Simulated results of liquid phase spray in constant-volume vessel at an ambient gas temperature of Ta = 950 K, an ambient gas density of ρa = 60 kg/ m3,and an injection time of 0.5 ms after the start of injection
Fig.7  Effect of liquid breakup models on numerical results for isosurface of turbulent kinetic energy ( κ , κ = 150 J/kg) of ambient gas in constant-volume vessel
Engine speed Start of injection/(˚) ATDC Injection duration EGR/% Intake pressure/kPa Intake temperature/K
821 –9 5.5˚ 48.34 103 393
Tab.6  Engine operating conditions for experimental study conducted by Klingbeil, et al. [17]
Fig.8  Comparison of the present numerical simulation employing different liquid breakup models with experimental results obtained by Klingbeil, et al. [17]

(a) In-cylinder pressure history; (b) heat release rates (HRR)

Fig.9  Numerically simulated distributions of in-cylinder equivalence ratio and simulated in-cylinder spray at a crank angle of –5˚ ATDC
Fig.10  Comparison of soot and NOx emissions between present numerical simulation employing different liquid breakup models and experimental results obtained by Klingbeil, et al. [17]
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