Fluidelastic effects may be responsible for instabilities of heat exchanger tubes when the fluid flow reaches the critical velocity. The fluidelastic phenomenon is usually studied on experimental mock-ups, which may display only one critical velocity. In this paper, a method based on active vibration control is proposed in order to derive several critical velocities for fluidelastic instability corresponding to several different values of damping, which is artificially varied on the same mock-up. Experimental tests are performed on a flexible tube equipped with piezoelectric actuators in a rigid array under air-water cross-flow. It is shown that the reduced critical velocities thus obtained fit well in a classical stability map. [S0739-3717(00)01603-2]

1.
Connors, H.J., 1970, “Fluid-elastic vibration of tube arrays excited by cross-flow,” Proceedings, Flow-induced vibration in heat exchanger, ASME, Chicago, New York, pp. 42–46.
2.
Chen
,
S.S.
,
1987
, “
A general theory for dynamic instability of tube arrays in cross-flow
,”
J. Fluids Struct.
,
1
, pp.
35
53
.
3.
Pettigrew
,
M.J.
, and
Taylor
,
C.E.
,
1994
, “
Two-phase flow-induced vibration: an overview
,”
ASME J. Pressure Vessel Technol.
,
116
, pp.
233
253
.
4.
Granger
,
S.
,
Campistron
,
R.
, and
Lebret
,
J.
,
1993
, “
Motion-dependent excitation mechanisms in a square in-line tube bundle subject to water cross-flow: an experimental modal analysis
,”
J. Fluids Struct.
,
7
, pp.
521
550
.
5.
Blevins, R.D., 1990, Flow-Induced vibration, 2nd ed., Van Nostrand Reinhold, New York.
6.
Price
,
S.J.
, and
Paı¨doussis
,
M.P.
,
1984
, “
An improved mathematical model for the stability of cylinder rows subject to cross-flow
,”
J. Sound Vib.
,
97
, pp.
615
640
.
7.
Lever
,
J.H.
, and
Weaver
,
D.S.
,
1982
, “
A theoretical model for fluidelastic instability in heat exchanger in tube bundles
,”
ASME J. Pressure Vessel Technol.
,
14
, pp.
147
158
.
8.
Fujita, K., Nakamura, T., Mureithi, N.W., and Ichioka, T., 1995, “Recent topics on cross-flow induced vibration of tube arrays,” Proceedings, Flow-Induced Vibration, ASME, New York, PVP-Vol. 298, pp. 45–54.
9.
Baz
,
A.
, and
Ro
,
J.
,
1991
, “
Active control of flow-induced vibrations of a flexible cylinder using direct velocity feedback
,”
J. Sound Vib.
,
146
, No.
1
, pp.
33
45
.
10.
Kaneko, S., and Hirota, K., 1992, “A study on active control of leakage flow induced vibrations,” Proceedings, Control of Flow-Induced Vibration, Vol. III, pp. 63–69.
11.
Preumont, A., 1997, Vibration Control of Active Structures: An Introduction, Lausanne (Ch.): Presses Polytechniques et Universitaires Romandes.
12.
Meskell, C., and Fitzpatrick, J.A., 1997, “Identification of linearised parameters for fluidelastic instability,” Proceedings, Fluid-Structure Interaction, Aeroelasticity, Flow-Induced Vibration and Noise, ASME, New York, AD-Vol. 53-1, pp. 319–324.
13.
Granger
,
S.
,
1990
, “
A new signal processing method for investigating fluidelastic phenomena
,”
J. Fluids Struct.
,
4
, pp.
73
97
.
14.
Caillaud
,
S.
,
de Langre
,
E.
, and
Piteau
,
P.
,
1999
, “
The measurement of fluidelastic forces in tube bundles using piezoelectric actuators
,”
ASME J. Pressure Vessel Technol.
,
121
, pp.
232
238
.
15.
Pettigrew
,
M.J.
,
Taylor
,
C.E.
, and
Kim
,
B.S.
,
1989
, “
Vibration of tubes bundles in two-phase cross-flow, Part 1: hydrodynamic mass and damping
,”
ASME J. Pressure Vessel Technol.
,
111
, pp.
466
477
.
16.
Axisa
,
F.
,
Antunes
,
J.
, and
Villard
,
B.
,
1990
, “
Random excitation of heat exchanger tubes by cross-flows
,”
J. Fluids. Struct.
,
4
, pp.
321
341
.
17.
Hadj-Sadok, C., de Langre, E., and Granger, S., 1995, “Inverse methods for the measurement of fluid-elastic forces in tube bundles,” Proceedings, Flow-Induced Vibration, 6th Int. Conf., London, Rotterdam: Bearman Ed., pp. 363–371.
18.
de Langre
,
E.
, and
Villard
,
B.
,
1998
, “
An upper bound on random buffeting forces caused by two-phase flows across tubes
,”
J. Fluids Struct.
,
12
, pp.
1005
1023
.
19.
Crawley
,
E.F.
, and
De Luis
,
J.
,
1987
, “
Use of piezoelectric actuators as elements of intelligent structures
,”
Am. Inst. Aeronaut. Astronaut. J.
,
25
, No.
10
, pp.
1373
1385
.
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