European Journal of Mechanics B/Fluids 58 (2016) 109–116
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European Journal of Mechanics B/Fluids
journal homepage: www.elsevier.com/locate/ejmflu
Alternative interpretation of the Superpipe data and motivation for
CICLoPE: The effect of a decreasing viscous length scale
Ricardo Vinuesa
a,b,∗
, Richard D. Duncan
b
, Hassan M. Nagib
b
a
Linné FLOW Centre, KTH Mechanics, Osquars Backe 18, Stockholm, Sweden
b
Department of Mechanical, Materials and Aerospace Engineering (MMAE), Illinois Institute of Technology (IIT), Chicago, IL, 60616, USA
article info
Article history:
Received 21 October 2015
Received in revised form
11 February 2016
Accepted 31 March 2016
Available online 19 April 2016
Keywords:
Experimental limitations
Wall-bounded turbulence
Pitot tubes
Superpipe
CICLoPE
abstract
Pressurization and cryogenic conditions have been used in some experiments to change the kinematic
viscosity ν of the flowing gas by many orders of magnitude in order to achieve high Reynolds number
conditions in facilities of limited size. This leads to a substantial reduction of the viscous length scale ℓ
∗
=
ν/u
τ
, as in the so-called Princeton ‘‘Superpipe’’ experiments. We demonstrate that the limited dimensions
of the facilities and probes can lead to inaccuracies in the near-wall measurements for increasing Reynolds
number. Specifically, a lack of accurate wall-normal probe positioning is simulated using three different
datasets of wall-bounded turbulent flows. Relatively large errors in the overlap region parameters are
observed for position errors of small physical magnitude that become greatly amplified in wall units as ℓ
∗
is reduced. This offers an alternative interpretation to some of the key findings reported by the Superpipe
team, such as the increasing lower limit of the logarithmic region y
+
log,min
, the existence of a power law
region between the wall and the logarithmic layer, and the ‘‘mixing transition’’ phenomenon in wall-
bounded turbulence.
© 2016 Elsevier Masson SAS. All rights reserved.
1. Introduction
High Reynolds numbers in wall-bounded turbulent flows are
often reached by increasing the characteristic length and/or ve-
locity scale. Both can usually be modified in boundary layer ex-
periments, since the characteristic length is the distance from the
leading edge x, and the characteristic velocity is the freestream ve-
locity U
∞
. However, the characteristic length is fixed by the size
of the facility in most fully-developed channel and pipe flows (as
the height of the channel H and the pipe diameter D respectively),
with only the bulk velocity U
b
and kinematic viscosity ν variable.
To avoid compressibility effects, some experiments overcame the
limited physical dimensions through manipulation of ν . In these
experiments, the facility is pressurized well above atmosphere to
reduce the value of ν significantly, so that very high Reynolds num-
ber conditions can be obtained. This technique was used in the
Superpipe experiments, where Reynolds numbers based on bulk
velocity and pipe diameter up to Re
D
= 35 × 10
6
were achieved
[1,2]. The mean velocity profile in this experiment was first stud-
∗
Corresponding author at: Linné FLOW Centre, KTH Mechanics, Osquars Backe
18, Stockholm, Sweden.
E-mail address: rvinuesa@mech.kth.se (R. Vinuesa).
ied by Zagarola and Smits [1], who presented measurements for
Reynolds numbers from Re
D
= 0.031 × 10
6
to 35 × 10
6
using a
0.9 mm diameter probe. They reported the existence of two over-
lap regions: a power law for 60 < y
+
< 500 and a logarithmic
region for 600 < y
+
< 0.07R
+
when Re
D
> 0.4 × 10
6
. Here,
R = D/2 is the pipe radius and y
+
is the wall-normal coordinate
normalized by the viscous length scale ℓ
∗
= ν/u
τ
. The friction ve-
locity u
τ
=
√
τ
w
/ρ (where τ
w
is the mean shear stress at the wall
and ρ is the fluid density) is used to normalize the mean velocity
U , to form U
+
= U /u
τ
. For the classical law of the wall [3] or ‘‘log
law’’ given by:
U
+
=
1
κ
ln(y
+
) + B, (1)
they reported the values κ = 0.436 and B = 6.15 for the constants.
McKeon et al. [2] performed new experiments in the same
Reynolds number range using a 0.3 mm diameter probe, and
analyzed both sets of data using new static pressure corrections [4].
Their study showed significant changes from the previous analysis:
a power law region was found for 50 < y
+
< 300, and the
log region was found for 600 < y
+
< 0.12R
+
when Re
D
>
0.2 × 10
6
. The values of the constants were modified to κ =
0.421 and B = 5.6. Nagib and Chauhan [5] recently showed that
the Superpipe experiments exhibit an increasing lower limit of
http://dx.doi.org/10.1016/j.euromechflu.2016.03.010
0997-7546/© 2016 Elsevier Masson SAS. All rights reserved.