The cavitation phenomenon interests a wide range of machines, from internal combustion engines to turbines and pumps of all sizes. It affects negatively the hydraulic machines’ performance and may cause materials’ erosion. The cavitation, in most cases, is a phenomenon that develops at a constant temperature, and only a relatively small amount of heat is required for the formation of a significant volume of vapor, and the flow is assumed isothermal. However, in some cases, such as thermosensible fluids and cryogenic liquid, the heat transfer needed for the vaporization is such that phase change occurs at a temperature lower than the ambient liquid temperature. The focus of this research is the experimental and analytical studies of the cavitation phenomena in internal flows in the presence of thermal effects. Experiments have been done on water and nitrogen cavitating flows in orifices at different operating conditions. Transient growth process of the cloud cavitation induced by flow through the throat is observed using high-speed video images and analyzed by pressure signals. The experiments show different cavitating behaviors at different temperatures and different fluids; this is related to the bubble dynamics inside the flow. So to investigate possible explanations for the influence of fluid temperature and of heat transfer during the phase change, initially, a steady, quasi-one-dimensional model has been implemented to study an internal cavitating flow. The nonlinear dynamics of the bubbles has been modeled by Rayleigh–Plesset equation. In the case of nitrogen, thermal effects in the Rayleigh equation are taken into account by considering the vapor pressure at the actual bubble temperature, which is different from the liquid temperature far from the bubble. A convective approach has been used to estimate the bubble temperature. The quasisteady one-dimensional model can be extensively used to conduct parametric studies useful for fast estimation of the overall performance of any geometric design. For complex geometry, three-dimensional computational fluid dynamic (CFD) codes are necessary. In the present work good agreements have been found between numerical predictions by the CFD FLUENT code, in which a simplified form of the Rayleigh equation taking into account thermal effects has been implemented by external user routines and some experimental observations.

1.
Franc
,
J. P.
, and
Michel
,
J. M.
, 2004,
Fundamentals of Cavitation
,
Kluwer Academic
,
Dordrecht, The Netherlands
.
2.
Utturkar
,
Y.
,
Wu
,
J.
,
Wang
,
G.
, and
Shyy
,
W.
, 2005, “
Recent Progress in Modeling of Cavitation for Liquid Rocket Propulsion
,”
Prog. Aerosp. Sci.
0376-0421,
41
, pp.
558
608
.
3.
Song
,
C. C. S.
, and
Qin
,
Q.
, 2001, “
Numerical Simulation of Unsteady Cavitation Flows
,”
Proceedings of the CAV 2001: Fourth International Symposium on Cavitation
, Pasadena, CA, Jun. 20–23.
4.
Senocak
,
I.
, and
Shyy
,
W.
, 2002, “
A Pressure-Based Method for Turbulent Cavitating Flow Computations
,”
J. Comput. Phys.
0021-9991,
176
(
2
), pp.
363
383
.
5.
Singhal
,
A. K.
,
Athavale
,
M. M.
, and
Jiang Yu Li
,
H.
, 2002, “
Mathematical Basis and Validation of the Full Cavitation Model
,”
ASME J. Fluids Eng.
0098-2202,
124
, pp.
617
624
.
6.
De Giorgi
,
M. G.
,
Rodio
,
M. G.
, and
Ficarella
,
A.
, 2008, “
Cavitation Modeling in Cryogenic Fluids for Liquid Rocket Engine Applications
,”
AIAA 38th Fluid Dynamics Conference and Exhibit
, Seattle, WA, Jun. 23–26, Paper No. AIAA-2008-3842.
7.
Franc
,
J. P.
,
Rebattet
,
C.
, and
Coulon
,
A.
, 2004, “
An Experimental Investigation of Thermal Effect in a Cavitating Inducer
,”
ASME J. Fluids Eng.
0098-2202,
126
, pp.
716
723
.
8.
He
,
L.
, and
Ruiz
,
F.
, 1995, “
Effect of Cavitation on Flow and Turbulence in Plain Orifices for High-Speed Atomization
,”
Atomization Sprays
1044-5110,
5
, pp.
569
584
.
9.
Tamaki
,
N.
,
Shimizu
,
M.
,
Nishida
,
K.
, and
Hiroyasu
,
H.
, 1998, “
Effects of Cavitation and Internal Flow on Atomization of a Liquid Jet
,”
Atomization Sprays
1044-5110,
2
, pp.
179
197
.
10.
Tamaki
,
N.
,
Shimizu
,
M.
, and
Hiroyasu
,
H.
, 2001, “
Enhancement of the Atomization of a Liquid Jet by Cavitation in a Nozzle Hole
,”
Atomization Sprays
1044-5110,
11
(
2
), pp.
125
137
.
11.
Ahn
,
K.
,
Kim
,
J.
, and
Yoon
,
Y.
, 2006, “
Effects of Orifice Internal Flow on Transverse Injection Into Subsonic Crossflows: Cavitation and Hydraulic Flip
,”
Atomization Sprays
1044-5110,
16
(
1
), pp.
15
34
.
12.
Wang
,
Y. -C.
, and
Brennen
,
C. E.
, 1998, “
One-Dimensional Bubbly Cavitating Flows Through a Converging-Diverging Nozzle
,”
ASME J. Fluids Eng.
0098-2202,
120
, pp.
166
170
.
13.
Brennen
,
C. E.
, 1995,
Cavitation and Bubble Dynamics
,
Oxford University Press
,
New York
.
14.
Brennen
,
C. E.
, 1994,
Hydrodynamics of Pumps
,
Oxford University Press
,
New York
.
15.
Ivashnev
,
O. E.
, and
Smirnov
,
N. N.
, 2004, “
Thermal Growth of a Vapor Bubble Moving in a Superheated Liquid
,”
Fluid Dyn.
0015-4628,
39
(
3
), pp.
414
428
.
16.
Davis
,
M. P.
,
Dunn
,
P. F.
, and
Thomas
,
F. O.
, 2007, “
Draft: Jet Fuel Cavitation in a Converging Diverging Nozzle
,”
Proceedings of the FEDSM2007, Fifth Joint ASME/JSME Fluids Engineering Conference
, San Diego, CA, Jul. 30–Aug. 2.
17.
De Giorgi
,
M. G.
,
Ficarella
,
A.
, and
Laforgia
,
D.
, 2007, “
Modeling Nucleation Phenomena in Cavitating Flow
,”
18th AIAA Computational Fluid Dynamics Conference and Exhibit
, Miami, FL, Jun. 25–28.
18.
Cervone
,
A.
,
Bramanti
,
C.
,
Rapposelli
,
E.
, and
d’Agostino
,
L.
, 2006, “
Thermal Cavitation Experiments on a NACA 0015 Hydrofoil
,”
ASME J. Fluids Eng.
0098-2202,
128
(
2
), pp.
326
331
.
19.
Gustavsson
,
J. P. R.
,
Denning
,
K. C.
, and
Segal
,
C.
, 2008, “
Hydrofoil Cavitation Under Strong Thermodynamic Effect
,”
ASME J. Fluids Eng.
0098-2202,
130
(
9
), pp.
091303
091308
.
20.
Simoneau
,
R. J.
, and
Hendricks
,
R. C.
, 1979, “
Two-Phase Choked Flow of Cryogenic Fluids in Converging-Diverging Nozzles
,” Report No. NASA TP 1484.
21.
Tani
,
N.
, and
Nagashima
,
T.
, 2003, “
Cryogenic Cavitating Flow in 2D Laval Nozzle
,”
J. Therm. Sci.
1003-2169,
12
, pp.
157
161
.
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