Results are presented on the behavior of the turbulent wake behind a submarine model for a range of Reynolds numbers based on the model length between 0.49×106 and 1.8×106, for test locations between 3 and 9 diameters downstream of the stern. The shape of the model emulates an idealized submarine, and tests were performed with and without stern fins. In the absence of fins, the velocity profile in planes away from the influence of the sail rapidly becomes self-similar and is well described by a function of exponentials. The fins create defects in the velocity profiles in the outer region of the wake, while yielding higher values of turbulence at locations corresponding to the tips of the fins. Measurements conducted in planes away from the midline plane show that the velocity profiles remain self-similar, while the shear stress profiles clearly show the effects of the necklace vortices trailing from the base of the fins.

1.
Townsend
,
A. A.
, 1956,
The Structure of Turbulent Shear Flow
,
Cambridge University Press
,
Cambridge, England
.
2.
Wygnanski
,
I.
,
Champagne
,
F.
, and
Marasli
,
B.
, 1986, “
On the Large Scale Structures in Two Dimensional, Small Deficit Turbulent Wakes
,”
J. Fluid Mech.
0022-1120,
168
, pp.
31
71
.
3.
Johansson
,
P. B. V.
, and
George
,
W. K.
, 2006, “
The Far Downstream Evolution of the High-Reynolds-Number Axisymmetric Wake Behind a Disk. Part 1. Single-Point Statistics
,”
J. Fluid Mech.
0022-1120,
555
, pp.
363
385
.
4.
Chevray
,
R.
, 1968, “
The Turbulent Wake of a Body of Revolution
,”
ASME J. Basic Eng.
0021-9223,
90
, pp.
275
284
.
5.
Sirviente
,
A. I.
, and
Patel
,
V. C.
, 1999, “
Experiments in the Turbulent Near Wake of an Axisymmetric Body
,”
AIAA J.
0001-1452,
37
(
12
), pp.
1670
1673
.
6.
Huang
,
T.
,
Liu
,
H. L.
,
Groves
,
N.
,
Forlini
,
T.
,
Blanton
,
J.
, and
Gowing
,
S.
, 1992, “
Measurements of Flows Over an Axisymmetric Body With Various Appendages in a Wind Tunnel: The DARPA Suboff Experimental Program
,”
Proceedings of the 19th Symposium on Naval Hydrodynamics
, Seoul, Korea.
7.
Simpson
,
R. L.
, 2001, “
Junction Flows
,”
Annu. Rev. Fluid Mech.
0066-4189,
33
, pp.
415
443
.
8.
Groves
,
N. C.
,
Huang
,
T. T.
, and
Chang
,
M. S.
, 1989, “
Geometric Characteristics of DARPA SUBOFF Models
,” David Taylor Research Center, Bethesda, MD, Technical Report No. DTRC/SHD-1298-01.
9.
Jiménez
,
J. M.
, 2007, “
High Reynolds Number Flows About Bodies of Revolution With Application to Submarines and Torpedoes
,” Ph.D. thesis, Princeton University, Princeton, NJ.
10.
Reynolds
,
R.
, 2003, “
An Experimental Study of Axisymmetric Wakes (With Application to Submarines)
,” MS thesis, Princeton University, Princeton, NJ.
11.
Sato
,
H.
, and
Kuriki
,
K.
, 1961, “
The Mechanism of Transition in the Wake of a Thin Flat Plate Placed Parallel to a Uniform Flow
,”
J. Fluid Mech.
0022-1120,
11
, pp.
321
352
.
12.
Patel
,
V. C.
,
Nakayama
,
A.
, and
Damian
,
R.
, 1974, “
Measurements in the Thick Axisymmetric Turbulent Boundary Layer Near the Tail of a Body of Revolution
,”
J. Fluid Mech.
0022-1120,
63
, pp.
345
367
.
13.
Merz
,
R. A.
,
Yi
,
C. H.
, and
Przirembel
,
C. E. G.
, 1986, “
Turbulence Intensities in the Near-Wake of a Semielliptical Afterbody
,”
AIAA J.
0001-1452,
24
, pp.
2038
2040
.
14.
Ramaprian
,
B. R.
, and
Patel
,
V. C.
, 1982, “
The Symmetric Turbulent Wake of a Flat Plate
,”
AIAA J.
0001-1452,
20
, pp.
1228
1235
.
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