The flow downstream of a three-dimensional double backward facing step (3D DBWFS) is investigated for Reynolds number Reh ranging from 5×103 to8×104 (based on the first step height h). The flow is studied both qualitatively by means of laser tomoscopy and oil-flow visualizations and quantitatively by means of particle image velocimetry (PIV) measurements. In particular, the results show a mean flow asymmetry. A sensitivity study around zero degree sideslip has shown that the flow is bistable for this geometry. This bistability has been observed in two different wind tunnels for very different upstream conditions. As a main consequence, the zero degree drift angle could be a relevant validation case of unstable flow computation. More tests are carried out to understand and control this particular flow feature.

References

1.
Eaton
,
J.
, and
Johnston
,
J.
, 1981, “
A Review of Research on Subsonic Turbulent Flow Reattachment
,”
AIAA J.
,
19
(
9
), pp.
1093
1100
.
2.
Syms
,
G.
, 2008, “
Simulation of Simplified-Frigate Airwakes Using a Lattice-Boltzmann Method
,”
J. Wind. Eng. Ind. Aerodyn.
,
96
(
6
), pp.
1197
1206
.
3.
Cheney
,
B.
, and
Zan
,
S.
, 1999, “
CFD Code Validation Data and Flow Topology for the Technical Co-operation Program AER-TP2 Simple Frigate Shape
,”
Tech. Rep.
LTR-A-035, NRC-CNRC.
4.
Tinney
,
C.
, and
Ukeiley
,
L.
, 2009, “
A Study of a 3-D Double Backward-Facing Step
,”
Exp. Fluids
,
47
(
3
), pp.
427
438
.
5.
Schlichting
,
H.
, and
Gersten
,
K.
, 2000,
Boundary-Layer Theory
, 8th ed.,
Springer
,
Berlin
.
6.
Tai
,
T.
, 2001, “
Airwake Simulation of Modified TTCP/SFS Ship
,” in
RTO Applied Vehicle Technology Panel (AVT) Symposium
.
7.
Wakefield
,
N.
,
Newman
,
S.
, and
Wilson
,
P.
, 1998, “
CFD Predictions of the Influence of External Airflow on Helicopter Operations When Operating From Ship Flight Decks
,” in
RTO AVT Symposium on Fluid Dynamics Problems of Vehicles Operating Near or in the Air-Sea Interface
,
Research and Technology Organization
, pp.
2.1
2.10
.
8.
Reddy
,
K.
,
Toffoletto
,
R.
, and
Jones
,
K.
, 2000, “
Numerical Simulation of Ship Airwake
,”
Comput. Fluids
,
29
(
4
), pp.
451
465
.
9.
Liu
,
J.
, and
Long
,
L.
, 1998, “
Higher Order Accurate Ship Airwake Predictions for the Helicopter/Ship Interface Problem
,” in
Annual Forum Proceedings American Helicopter Society, Vol. 1 of Proceedings of the 54th Annual Forum Part 2 (of 2)
, pp.
58
70
.
10.
Castro
,
I.
, and
Dianat
,
M.
, 1983, “
Surface Flow Patterns on Rectangular Bodies in Thick Boundary Layers
,”
J. Wind. Eng. Ind. Aerodyn.
,
11
(
1–3
), pp.
107
119
.
11.
Kim
,
K.
,
Ji
,
H.
, and
Seong
,
S.
, 2003, “
Flow Structure Around a 3-D Rectangular Prism in a Turbulent Boundary Layer
,”
J. Wind. Eng. Ind. Aerodyn.
,
91
(
5
), pp.
653
669
.
You do not currently have access to this content.