The present paper illustrates the setup and the preliminary results of an experimental investigation of cavitation flow instabilities carried out by means of a high-speed camera on a three-bladed inducer in the cavitating pump rotordynamic test facility (CPRTF) at Alta S.p.A. The brightness thresholding technique adopted for cavitation recognition is described and implemented in a semi-automatic algorithm. In order to test the capabilities of the algorithm, the mean frontal cavitating area has been computed under different operating conditions. The tip cavity length has also been evaluated as a function of time. Inlet pressure signal and video acquisitions have been synchronized in order to analyze possible cavitation fluid-dynamic instabilities both optically and by means of pressure fluctuation analysis. Fourier analysis showed the occurrence of a cavity length oscillation at a frequency of 14.7Hz, which corresponds to the frequency of the rotating stall instability detected by means of pressure oscillation analysis.

1.
Stripling
,
L. B.
, and
Acosta
,
A. J.
, 1962, “
Cavitation in Turbopumps—Part 1
,”
ASME J. Basic Eng.
0021-9223,
84
, pp.
326
338
.
2.
Brennen
,
C. E.
, 1994,
Hydrodynamics of Pumps
, Concepts ETI, Inc. and
Oxford University Press
,
Norwich, VT
.
3.
Cervone
,
A.
,
Testa
,
R.
,
Bramanti
,
C.
,
Rapposelli
,
E.
, and
d’Agostino
,
L.
, 2005, “
Thermal Effects on Cavitation Instabilities in Helical Inducers
,”
J. Propul. Power
0748-4658,
21
(
5
), pp.
893
899
.
4.
Cervone
,
A.
,
Torre
,
L.
,
Bramanti
,
C.
,
Rapposelli
,
E.
, and
d’Agostino
,
L.
, 2006, “
Experimental Characterization of Cavitation Instabilities in a Two-Bladed Axial Inducer
,”
J. Propul. Power
0748-4658,
22
(
6
), pp.
1389
1395
.
5.
Tsujimoto
,
Y.
,
Yoshida
,
Y.
,
Maekawa
,
Y.
,
Watanabe
,
S.
, and
Hashimoto
,
T.
, 1997, “
Observations of Oscillating Cavitation of an Inducer
,”
ASME J. Fluids Eng.
0098-2202,
119
, pp.
775
781
.
6.
Kamijo
,
K.
,
Shimura
,
T.
, and
Tsujimoto
,
Y.
, 1994, “
Experimental and Analytical Study of Rotating Cavitation
,”
Proc. of ASME Cavitation and Gas-Liquid Flow in Fluid Machinery and Devices
, Lake Tahoe, NV, Jun. 19–23.
7.
Hashimoto
,
T.
,
Yoshida
,
M.
,
Watanabe
,
M.
,
Kamijo
,
K.
, and
Tsujimoto
,
Y.
, 1997, “
Experimental Study of Rotating Cavitation of Rocket Propellant Pump Inducers
,”
J. Propul. Power
0748-4658,
13
(
4
), pp.
488
494
.
8.
Jousselin
,
F.
,
Courtot
,
Y.
,
Coutier-Delgosha
,
O.
, and
Reboud
,
J. L.
, 2001, “
Cavitating Inducer Instabilities: Experimental Analysis and 2D Numerical Simulation of Unsteady Flow in Blade Cascade
,”
Proc. of CAV2001—4th International Symposium on Cavitation
, Pasadena, CA, Jun. 20–23.
9.
Rapposelli
,
E.
,
Cervone
,
A.
, and
d’Agostino
,
L.
, 2002, “
A New Cavitating Pump Rotordynamic Test Facility
,”
Proc. of AIAA Joint Propulsion Conference and Exhibit
, Indianapolis, IN, Jul. 7–10, paper No. 2002-4285.
10.
Gonzalez
,
R. C.
, and
Woods
,
R. E.
, 2002,
Digital Image Processing
,
Prentice-Hall
,
New Jersey
.
11.
Kato
,
K.
,
Matudaira
,
Y.
, and
Obara
,
H.
, 2003, “
Flow Visualization of Cavitation With Particle and Bubble Image Processing
,”
Proc. of ASME FEDSM—Fluids Engineering Division Summer Meeting
, Honolulu, HI, Jul. 6–11.
12.
Otsu
,
N.
, 1979, “
A Threshold Selection Method From Gray-Level Histograms
,”
IEEE Trans. Syst. Man Cybern.
0018-9472,
9
(
1
), pp.
62
66
.
13.
Brennen
,
C. E.
, and
Acosta
,
A. J.
, 1973, “
Theoretical, Quasistatic Analyses of Cavitation Compliance in Turbopumps
,”
J. Spacecr. Rockets
0022-4650,
10
(
3
), pp.
175
180
.
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