The process of formation of air core and its development with time, inside one cylindrical and one conical nozzle having two tangential entries, has been analyzed experimentally and numerically. Experiments have been carried out using Plexiglas nozzles and water in ambient air; the air core has then been photographed for different nozzles and flow parameters. Numerical simulations have been performed using a finite volume method that employs unstructured grids with cell-wise local refinement and an interface-capturing scheme to predict the shape of the air core. The shape of the air core inside the cylindrical nozzle is found to be helicoidal at steady state for higher inlet velocity, whereas the shape of the free surface remains nearly cylindrical for low inlet velocity. In the conical nozzle, the air core is nearly axisymmetric in experiments. So only two-dimensional simulations are performed; the air core widens at the end of conical section as it approaches nozzle exit. For both nozzles numerical simulation predicts qualitatively and to a large extent also quantitatively the correct shape of the air core and the angle of the spray at the nozzle exit, as verified by comparisons with experimentally observed shapes.

1.
Chang
,
K. C.
,
Wnag
,
M. R.
,
Wu
,
W. J.
, and
Hong
,
C. H.
,
1993
, “
Experimental and Theoretical Study on Hollow-Cone Spray
,”
J. Propul. Power
,
9
, No.
1
, pp.
28
34
.
2.
Chen
,
S. K.
,
Lefebvre
,
A. H.
, and
Rollbuhler
,
J.
,
1993
, “
Factors Influencing the Circumferential Liquid Distribution from Pressure Swirl Atomizers
,”
ASME J. Eng. Gas Turbines Power
,
115
, pp.
447
452
.
3.
Datta
,
A.
, and
Som
,
S. K.
,
2000
, “
Numerical Predictions of Air Core Diameter, Coefficient of Discharge and Spray Cone Angle in a Swirl Spray Nozzle
,”
Int. J. Heat Fluid Flow
,
21
, pp.
412
419
.
4.
Kutty, S. P., Narashimhan, M., and Narayanaswamy, K., 1978, “Design and Prediction of Discharge Rate, Cone Angle and Air Core Diameter of Swirl Chamber Atomizers,” Proc. 1st Int. Conf. on Liquid Atomization and Spray Systems, pp. 93–100.
5.
Rizk
,
N. K.
, and
Lefebvre
,
A. H.
,
1985
, “
Internal Flow Characteristics of Simplex Swirl Atomizers
,”
AIAA J. of Propul. and Power
,
1
, No.
3
, pp.
193
199
.
6.
Rizk, N. K., and Lefebvre, A. H., 1985, “Prediction of Velocity Coefficient of Spray Cone Angle for Simplex Swirl Atomizers,” Proc. 3rd Int. Conf. On Liquid Atomization and Spray Systems, pp. 111C/2/1–16.
7.
Som
,
S. K.
, and
Mukherjee
,
S. G.
,
1980
, “
Theoretical and Experimental Investigations on the Formation of Air Core in a Swirl Atomizing Nozzle
,”
Appl. Sci. Res.
,
36
, pp.
173
176
.
8.
Som
,
S. K.
,
1983
, “
Theoretical and Experimental Studies on the Formation of Air Core in a Swirl Spray Atomizing Nozzle Using a Power Law Non-Newtonian Liquid
,”
Appl. Sci. Res.
,
40
, pp.
71
91
.
9.
Som
,
S. K.
, and
Biswas
,
G.
,
1984
, “
Initiation of Air Core in a Swirl Nozzle Using Power Law Fluids
,”
Acta Mech.
,
51
, pp.
179
197
.
10.
Suyari
,
M.
, and
Lefebvre
,
A. H.
,
1986
, “
Film Thickness Measurements in a Simlex Swirl Atomizer
,”
AIAA J. of Propul. and Power
,
2
, No.
6
, pp.
528
533
.
11.
Lafaurie
,
B.
,
Nardone
,
C.
,
Scardovelli
,
R.
,
Zaleski
,
S.
, and
Zanetti
,
G.
,
1994
, “
Modelling merging and fragmentation in multiphase flows with SURFER
,”
J. Comput. Phys.
,
113
, pp.
134
147
.
12.
Ubbink, O., 1997, “Numerical prediction of two fluid systems with sharp interfaces,” PhD thesis, University of London.
13.
Muzaferija, S., and Peric, M., 1999, “Computation of Free Surface Flow Using Interface-Tracking and Interface-Capturing Methods,” Chap. 2, O. Mahrenholtz and M. Markiewicz, eds., Nonlinear Water Wave Interaction, pp. 59–100, WIT Press, Southampton.
14.
Brackbill
,
J. U.
,
Kothe
,
D. B.
, and
Zemaach
,
C.
,
1992
, “
A continuum method for modeling surface tension
,”
J. Comput. Phys.
,
1
, pp.
335
354
.
15.
Patankar
,
S. V.
, and
Spalding
,
D. B.
,
1972
, “
A calculation procedure for heat, mass and momentum transfer in three-dimensional parabolic flows
,”
Int. J. Heat Mass Transf.
,
15
, pp.
1787
1806
.
16.
Comet User Manual, ICCM Institute of Computational Continuum Mechanics GmbH, Hamburg, Germany (www.iccm.de).
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