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VORTEX RING-LIKE STRUCTURES IN GASOLINE FUEL SPRAYS:
MODELLING AND OBSERVATIONS
Sergei SAZHIN*,
Felix KAPLANSKI**, Steven BEGG*, Morgan HEIKAL*
*Sir Harry Ricardo Laboratories, Internal Combustion Engines Group, School of Environment and Technology, Faculty of Science and Engineering, University of Brighton, Brighton, BN2 4GJ, UK
** Laboratory of Multiphase Physics, Tallinn University of Technology, Tallinn 19086, Estonia
2
Presentation overview
• VORTEX RING-LIKE STUCTURES IN ENGINES
• VORTEX RING MODELS• MODELLING VERSUS EXPERIMENTS• OTHER RECENT RESULTS
3
VORTEX RING-LIKE STUCTURES IN ENGINES
4
A typical spray in Diesel engines
5
Typical vortex ring-like structure in a gasoline fuel spray
Piston crown position
6
Schematic view of vortex ring generatorSchematic view of vortex ring generator ((Gharib Gharib et al.,et al.,1998 )1998 )
7
Formation stage (Gharib et al.,1998 )
L/D<4 L/D<4
L/D>4L/D>4
L/DL/D44‘‘optimal’ ringoptimal’ ring
8
Gasoline engine injectors
Injector A BFuel injector type Port (PFI) Direct (G-DI) Nominal fuel pressure 3.5 bar 100 barFuel temperature 22 °C 22 °CFuel type Iso-octane (2,2,4 TMP) Iso-octane (2,2,4 TMP)Injection frequency 1 Hz 1 HzInjection duration 5 ms 2 msAir pressure 1 bar 1 barAir temperature 20 °C 20 °C Orifice size 200 μm 250 μm
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VORTEX RING-LIKE STRUCTURE IS GASOLINE ENGINE
(injector A)
,
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VORTEX RING-LIKE STRUCTURE IS GASOLINE ENGINE
(injector B)
,
Injector axis
Penetration depth
Spray width
Vx1
Vx3
Vx2
2Ro
x
rl
11
The region of maximal vorticity
,
12
VORTEX RING MODELS
,
13
Schematic view of a vortex ring
Formulation of the problem
22
2
2
2 1
rrrrxu
xv
rt
,
)( tUrr
u 1
,,xr
v1
rrrxr
1
2
2
2
2 0
0002122
,:)(
,,,/rx
xx
0
2 dxdrrI
cb tRMAat
(t)x-xr
),,(,
, ,= ,= ,
00
03
0
0
dt
tdxtU
)()( 0
I
M
0R
=
ring-to-core radiusring-to-core radius
Approximate solution
11
Re][* b
c
t
b
22
2
2
2 1
*
20 /Re
..),,(Re),,(Re);,,( 21
..),,(Re),,(Re);,,( 21
, , I2
1exp 1
2221 3bc
122'*
btba.2/14/1 b
Velocity of the centroid at r=0
,
0
00
2
2
dxdrr
dxdrxr
x
dt
tdxVtU x
)()( 0
17
Velocity of the centroid at r=0
,
1222exp3
22
1
2 Iv
VU
n
xx
2
22 ;3,2
5;
2
3,
2
3 F
,;2
7,2;
2
5,
2
3
5
3 222
2
F
,!)()(
)()(;,;,
0 21
21212122
k kk
kkk
kbb
xaaxbbaaF
,;)(;1)( 10 ),2()1().........1()( kkk
,4
Γ
4,
0
030
20
RR
Mv
Rn
18
Velocity of the centroid at r=0 (short times)
,
),2/3(2
3ln
xU
,d
)(logd)(
x
xΓx
γ ≈ 0.57721566 is the Euler constant, ψ(x) is the di-gamma function
19
Velocity of the centroid at r=0 (long times)
,
.30
7 3xU
20
Velocity of the region of maximal vorticity
,
,d)(2
erfc2 01
0
2 JJUU xx
,d)exp(2
)(erfc 2
x
ttx
21
Velocity of the region of maximal vorticity at long
times
,
,2
1)(1 J
.d)()2
(erfc30
7 30
0
2
JU x
Θ 3 ~ t-3b 2/14/1 b
22
MODELLING VERSUS EXPERIMENTS
23
Velocity of the region of maximal vorticity
,
initial/ ttt
)(/)( initialtVtVV xxx
24
Velocity of the region of maximal vorticity
,
xV
25
Conclusions
1. A generalised vortex ring model is based on the assumption that the time dependence of the vortex ring thickness ℓ is given by the relation atb, where a is an arbitrary positive number, and 1/4 ≤b ≤ 1/2 is suggested.
2. The predictions of the model are compared with the results of experimental studies of vortex ring-like structures in gasoline engine-like conditions with a high pressure (100 bar) G-DI injector and a low-pressure (3.5 bar) port fuel injector (PFI). The G-DI results has shown good agreement with the model. In contrast, the agreement of the PFI results with the model has been poor.
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OTHER RECENT RESULTS
27
Transient heating of a semitransparent spherical body
Sazhin, S.S., Krutitskii, P.A., Martynov, S.B., Mason, D., Heikal, M.R., Sazhina, E.M. (2007) Transient heating of a semitransparent
spherical body, Int J Thermal Science, 46(5), 444-457.
22
( , )T T
R P t Rt R R R
/l l l lk c when R Rd
/g g g gk c when Rd<R<Rg
28
Evaporation of droplets into a background gas: kinetic modelling
Sazhin, S.S., Shishkova, I.N., Kryukov, A.P., Levashov, V.Yu., Heikal, M.R. (2007) Evaporation of droplets into a background gas: kinetic modelling, Int J Heat Mass Transfer, 50, 2675-2691.
1 2
Ts, s
x
TRd , Rd
Kinetic region
Hydrodynamic region
Rd
jV q
29
Approximate analysis of thermal radiation absorption in fuel droplets
22
( , )T T
R P t Rt R R R
/l l l lk c when R Rd
/g g g gk c when Rd<R<Rg
30
Approximate analysis of thermal radiation absorption in fuel droplets
Sazhin, S.S., Kristyadi T., Abdelghaffar, W.A., Begg, S., Heikal, M.R., Mikhalovsky, S.V., Meikle S.T., Al-Hanbali, O. (2007) Approximate analysis of thermal radiation absorption in fuel droplets, ASME J Heat Transfer, 129, 1246-1255.
6 43 10d
bd R l lR R
P R a R c
where θR is the radiation temperature, Rd is the droplet radius,
3 3 20 1 R 2 R= b + b /10 b ( /10 ) ,b
θR can be assumed equal to the external temperature Text in the case of an optically thin gas in the whole domain. The coefficients depend on the range of radii
0dR R
P R
3 3 20 1 R 2 R= a + a /10 a ( /10 ) ,a
31
Particle grouping in oscillating flows
.
Sazhin S.S., Shakked, T., Sobolev, V., Katoshevski, D. (2008) Particle grouping in oscillating flows, European J of Mechanics B/Fluids, 27, 131-149.
Katoshevski, D., Shakked, T., Sazhin, S.S., Crua, C., Heikal, M.R. (2008) Grouping and trapping of evaporating droplets in an oscillating gas flow, International J of Heat and Fluid Flow, 29, 415-426.
dgd uu
Std
du
1
Vd (m/s)
X (mm),
||3
4
dggD
dl
vvC
DSt
dgd uu
Std
du
1
Velocities are normalised by ω/k, the distance by 1/k and the time by 1/ω
32
Acknowledgements
The authors are grateful to EPSRC (Project EP/E047912/1) for financial support.
33
Thank you for your attention
Any comments or suggestions
would be highly appreciated
VORTEX RING-LIKE STRUCTURES IN GASOLINE FUEL SPRAYS:
MODELLING AND OBSERVATIONS
Sergei SAZHIN*,
Felix KAPLANSKI**, Steven BEGG*, Morgan HEIKAL*
*Sir Harry Ricardo Laboratories, Internal Combustion Engines Group, School of Environment and Technology, Faculty of Science and Engineering, University of Brighton, Brighton, BN2 4GJ, UK
** Laboratory of Multiphase Physics, Tallinn University of Technology, Tallinn 19086, Estonia
35