Pressure drop and mixing behaviour of non-Newtonian fluids in a static mixing unit.
Kumar, Gunjan ; Upadhyay, S.N.
INTRODUCTION
Static (or motionless) mixers have been applied as mixing devices
in liquid-liquid, gas-liquid, solid-liquid, and solid-solid systems
quite effectively since 1970s. Small overall space requirement, low
cost, low power consumption, absence of moving parts, short residence
time, near plug flow behaviour, good mixing, high heat and mass transfer
efficiencies, low shear rate, self-cleansing, and interchangeable or
disposable nature are the major advantages of these mixers over agitated vessels (Bor, 1971; Baker, 1991; Thakur et al., 2003). In cooling
processes using static mixers, skinning due to boundary-layer
solidification is alleviated because of better radial mixing (Baker,
1991). Static mixers are also efficient in reducing fouling and coking
and enhancing the heat transfer during oil and tar residue treatments.
Commercial static mixers have a wide variety of basic geometries
and in order to control their performance many adjustable parameters
need to be optimized for specific applications (Byrde et al., 1999).
Thakur et al. (2003) presented an exhaustive review on the
state-of-the-art of these mixers and highlighted the areas needing more
work particularly for systems involving viscous Newtonian and
non-Newtonian fluids.
Static mixer systems are widely used with complex fluids in the
polymer and food processing industries, but measurement of pressure drop
for non-Newtonian fluids has been the subject of only a few studies.
Limited reported data are available in the literature for viscous and
viscoelastic fluids (Shah and Kale, 1991, 1992; Chandra and Kale, 1992,
1995). Shah and Kale (1991, 1992) compared the data for viscoelastic
solutions of polyacrylamide with inelastic solutions of carboxymethyl
cellulose (CMC) and concluded that elasticity always increased the
friction factor. This is expected since elasticity is important in the
entrance region flow, and the sequential elements in a static mixer
system create a sequence of entrance region flows.
Shah and Kale (1991, 1992) correlated their pressure drop data for
polymeric fluids using friction factor and the Metzner-Reed generalized
Reynolds number defined as:
f = [DELTA][P.sub.sm][D.sub.t][[epsilon].sub.2]/2L[rho][u.sup.2]
(1)
and
Re = [rho][u.sup.2-n][D.sup.n.sub.t]/K[8.sup.n-1]
[[epsilon].sub.2-n] (2)
The parameter K is the consistency index and n is the flow
behaviour index of fluid. Li et al. (1997) suggested another definition
of Reynolds number which is more general. This generalized Reynolds
number is written as:
[Re.sub.g] = [rho]u[D.sub.t]/[[mu].sup.*] [epsilon] (3)
Here, [[mu].sup.*] is the apparent viscosity corresponding to the
shear rate at the wall.
This article presents the results of pressure drop and residence
time distribution experiments conducted with a new laboratory made
static mixer and four non-Newtonian fluids--aqueous solutions of CMC,
polyvinyl alcohol (PVA), and polyethylene glycol (PEG). The purpose has
been to come out with the design of a new motionless mixer which could
be easily fabricated and used in place of commercial mixers.
EXPERIMENTAL
Test Fluids
Aqueous solutions of CMC, PVA, and PEG were used as test fluids.
These solutions obey power-law model and do not suffer from thixotropy or change on aging.
CMC (medium viscosity) was obtained from Cellulose Products Ltd.
(Ahemadabad, India), CMC (high viscosity) from S. D. Fine Chemicals Ltd.
(Mumbai, India) and PVA (MW 10000) and PEG (MW 9000) from Lab-Chemical
Industry (Mumbai, India).
Test solutions of known concentrations were prepared by dissolving
the polymers in deionized water following the procedure used earlier
(Lal, 1980).
The rheological properties of all solutions were determined from
the flow-curves prepared using the flow and pressure drop data collected
with the help of a capillary tube viscometer as described earlier (Lal,
1980).
Static Mixer
The static mixer (MALAVIYA mixer) elements were fabricated in
laboratory using PMMA sheets and tubes. The diagram, dimensions, and
photograph of static mixer used in this work are shown in Figures 1 and
2, respectively. The S-shaped curved portions were made by cutting out
1/3rd part of a 0.0257 m PMMA tube and the discs were made from a 6 mm
thick PMMA sheet. Two curved parts were glued together to give S-shape
elements as well as to the disk by placing the glued segments radially
on either side of the disk. Such an attachment provided S-shaped
protrusions aligned diametrically on either side of the disk. A hole was
also drilled diametrically in the edge of the disk for ensuring proper
alignment of elements in the tube.
[FIGURE 1 OMITTED]
[FIGURE 2 OMITTED]
[FIGURE 3 OMITTED]
Experimental Set-Up
Experimental set-up used is shown in Figure 3. The test column was
made of a perspex tube of 0.042 m ID and 1.1 m length. Static elements
were suspended in the column with the help of copper wire of 1 mm
diameter, which was rigidly fixed at the two ends of the test pipe with
help of rubber corks. Open tube manometers were used for measuring the
pressure drop and the liquid flow rate was controlled using a calibrated
rotameter. Tank 1 contained the test fluid and Tank 2 was used for
storing the tracer--the NaCl solution prepared in the respective test
fluid. The samples of tracer bearing test fluid at the outlet end were
collected from the sampling port. Test fluids were pumped to the column
through a rotameter with the help of a centrifugal pump.
Experimental Procedure
Pressure drop measurement
Desired test fluid was taken in Tank 1 and pumped to the static
mixer unit from the bottom of the column. Pressure drop
([DELTA][P.sub.sm]=h[rho]g) at a given flow rate was calculated by
measuring the difference in liquid heights in the manometer tubes. Flow
rates were calculated by measuring the time for collecting 1 L of the
test fluid.
Friction factor f, was calculated from the pressure drop
[DELTA][P.sub.sm], diameter of tube [D.sub.t], fluid velocity u,
porosity [epsilon], density of fluid [rho], length of static elements
[L.sub.e], and number of static elements N. Reynolds number, Re was
calculated using the superficial velocity and rheological constants.
Void volume fraction, [epsilon] was calculated by measuring the volume
of water displaced due to static mixer. The average value of the void
fraction, [euro] was found to be 0.815.
RTD measurement
The RTD data were generated by injecting the tracer solution (NaCl
solution in the test fluid) into the test section at some time, t = 0
and then measuring the tracer concentration, C in the effluent stream as
a function of time. These experiments were performed with all the test
fluids by giving step input and pulse input of tracer to the static
mixer unit in separate runs. Concentrations were calculated by measuring
conductivity of the effluent stream with the help of a conductivity
meter and using the calibration graph. The calibration curves were
straight line when plotted as conductivity versus [square root of
(concentration)].
Cumulative distribution or F(t) versus t curves were drawn from the
RTD experimental data with step input of tracer for all test fluids.
Flow rate of test fluids was maintained constant at 1 L/min and the
tracer flow rates were maintained constant at 60 mL/min. The
conductivity values of solutions were converted into corresponding
concentrations from the standard curve. Then F(t) values were calculated
and cumulative distribution curves were drawn by plotting F(t) versus
[bar.t].
E(t) curves were drawn from the pulse input data. In this case 20
mL of NaCl solution was injected instantly into the static mixer column
and then the effluent NaCl conductivities were measured. These E(t)
versus t curves were used to compare the experimental results with the
proposed RTD model.
All measurements were performed with mixers having different
orientations of static elements, that is, 0[degrees], 45[degrees], and
90[degrees] with respect to each other.
RESULTS AND DISCUSSION
Rheological Properties
The rheological properties of 1% aqueous [CMC.sub.hv], 1.5% aqueous
[CMC.sub.mv], 4% aqueous PVA, and 10% aqueous PEG solutions were
determined with a capillary tube viscometer. The experiments were
carried out at a controlled temperature of 25[degrees]C. The values of
shear stress at the wall ([[tau].sub.w] = D[DELTA]P/4L) and the
corresponding pseudo-shear rate (8u/D) were calculated after correcting
the pressure gradient in the capillary tube viscometer for entrance
effect at the average fluid velocity. The rheological constants were
determined by fitting the power-law model to these plots.
The polymer solutions used were pseudoplastic in nature having flow
behaviour indices less than unity, which was one of the main
considerations for selecting these particular fluids for the present
study. The values of both K and n at a given temperature were found to
be constant in the range of shear stress studied. Rheological constants
for different test fluids and their density are given in Table 1.
Pressure Drop
Pressure drop estimation is the first parameter for selection of a
proper static mixer system. The basic equation for pressure drop during
flow of a homogeneous, isothermal, incompressible fluid in a circular
tube can be easily extended to that with static mixers and can be
written as:
[DELTA][P.sub.sm] = 2f[rho][u.sup.2]/[D.sub.t] L =
2f[rho][u.sup.2]/[D.sub.t] N[L.sub.e] (4)
or
f = [DELTA][P.sub.sm][D.sub.t] / 2NL[rho][u.sup.2] or f =
[DELTA][P.sub.sm][D.sub.e] / 2N[L.sub.e][rho][u.sup.2] (5)
Due to reduction in the cross-sectional area for flow, the average
superficial velocity of fluid through the static mixer system would be
higher than that for the empty column used for the mixer assembly. Hence
for static mixer some workers have replaced diameter [D.sub.t] with
hydraulic mean diameter, [D.sub.e]. Here N is the number of mixing
element and [L.sub.e] is the effective length of one element. The
friction factor, f is a function of Reynolds number and is determined
experimentally or by CFD method for a particular mixer.
The same general concepts apply to flow in static mixers as those
for the open tube except that the transition values for Re are lower by
a factor of about 2. Flow is generally laminar for Re < 50 and
turbulent for Re > 1000. The static inserts cause systematic
disturbances to the flow field so that complex but fairly reproducible
flow behaviour can be expected in the intermediate range 50 < Re <
1000. Actual range of transition, however, depends on the design of the
static elements including their aspect ratio. For helical and Kenics
mixer elements, this region begins at Re around 43 for
[L.sub.e]/[D.sub.e] [less than or equal to] 0.8, but is delayed to Re
[approximately equal to] 55 when [L.sub.e]/[D.sub.e] is 1 (Jaffer and
Wood, 1998). The influence of aspect ratio has been confirmed by Joshi
et al. (1995), who also concluded that low aspect ratios were better for
heat transfer. However, the set-up used for generating most of the
experimental data are for systems with aspect ratio of 1.5 (Rauline et
al., 1998, 2000). For Sulzer SMX elements, Li et al. (1997) reported
that the laminar regime prevails up to Re = 15 while the turbulent
regime begins when Re = 1000.
A convenient way of representing pressure drop data is to directly
correlate the friction factor with the Reynolds number. In laminar flow,
the classic relationship between f and Re is usually obtained as:
f = [C.sub.1]/Re (6)
where [C.sub.1] is a constant greater than 16. For laminar and
transition range it is:
f = [C.sub.1] / Re + [C.sub.2] / [Re.sup.m] (7)
The second term is intended to reflect the effect of radial flow
caused by the mixing elements. The values of [C.sub.1], [C.sub.2], and m
reported by earlier workers for various mixing elements are listed in
Table 2.
Owing to the limited use of static mixers in turbulent flow, fewer
correlations of pressure drop in this regime are available (Bourne et
al., 1992). Pahl and Muschelknautz (1982) and Cybulski and Werner (1986)
presented correlations for the friction factor for two ranges of
Reynolds number, 1200 < Re < 7000 and 7000 < Re < 30 000. A
typical correlation used for turbulent flow is of the form:
f = [C.sub.3] / [Re.sup.m'] (8)
where [C.sub.3] is a constant. The exponent m' itself has been
found to be a function of Reynolds number, typically decreasing at
higher values of Re. Cybulski and Werner (1986) presented results for
the Kenics, LPD and Komax mixers. At higher Reynolds numbers, m'
approaches 0 and f becomes constant. A similar behaviour is observed in
empty pipes with [f.sub.empty] [right arrow] 0.02 as Re [right arrow]
[infinity]. Limiting f values for Kenics, Hi-Toray, SMX, and SMV mixers
are 3, 11, 12, and 6-12, respectively (Pahl and Muschelknautz, 1982).
Figure 4 shows typical variation of friction factor, f with
Reynolds number, Re on logarithmic coordinates for all the fluids
studied and the three orientations used between two consecutive
elements. The line representing f-Re relation for empty tube is also
shown in these figures for comparison. It is seen that the pressure drop
in static mixer is about 3.5-5 times higher than that for empty tube.
From these plots it is also seen that for Re < 35, the log f varies
linearly with log Re. For Re > 35, upward deviation of f values from
the linear relation is observed indicating transition from the creeping
flow. The additional pressure losses are due to contributions from the
creeping flow as well as the boundary layer flow with in the transition
region. The secondary flows created in the direction perpendicular to
the main flow rather than the turbulence are attributed to be
responsible for the improved convective transfer in some cases of static
mixers (Morris and Proctor, 1977). Thus, the skin friction and to some
extent the form drag around the elements may contribute more to the
increased pressure drop (Shah and Kale, 1991).
A relation similar to Equation (7) can be used to correlate the
friction factor data. The constants [C.sub.1], [C.sub.2], and m for
various situations are reported in Table 2. It is revealed from Table 2,
that the new static mixer offers less pressure drop as compared to
Kenics and Sulzer static mixers. The correlation constants [C.sub.1] and
[C.sub.2] both are smaller compared to those for Kenics and Sulzer
static mixers and are nearly similar to those for the helical mixers. It
is also seen that the value of [C.sub.1] is higher for 45[degrees]
orientation of static elements. At 45[degrees] orientation of elements,
fluid streams split into four parts at the entrance and number of flow
paths increase in number as they proceed upward in static mixer, but at
0[degrees] and 90[degrees] orientation of static element, the fluid
streams split only into four parts at the entrance and remain in the
same situation in the following sections.
[FIGURE 4 OMITTED]
Residence Time Distribution
Mixing in static mixers is affected by scores of parameters.
Grosz-Roll (1980) tabulated more than 50. These parameters are not
always clearly defined and are also not easy to compare with each other.
There is no single criterion suitable for all applications, and each has
its advantages and disadvantages.
The RTD was determined experimentally by injecting NaCl tracer at
time t = 0 in the static mixer filled pipe and then measuring the tracer
concentration C, in the effluent stream as a function of time. These
experiments were performed for step input of tracer with all the test
fluids. Cumulative residence time distribution function, F(t), obtained
from a sudden step input of an inert tracer is a convenient parameter
for judging the mixing effectiveness of a system. The residence time
distribution data obtained are converted to F(t) values. Figures 4a,b
shows the cumulative distribution F(t) versus [bar.t] data for static
elements with 45[degrees] and 90[degrees] orientations as typical
example. Data for all test fluids with static elements at a particular
orientation are plotted on the same graph. Smoothed curves are also
drawn in these figures. The first appearance time, [[bar.t].sub.first]
of tracer is not exactly clear, however, it is slightly more than 0.5 in
each case. Figures 5a,b show that the first appearance time
([[bar.t].sub.first]) for 45[degrees] orientation of static elements is
slightly higher as compared to 90[degrees] orientation. This is due to
more complicated flow path provided by 45[degrees] orientation of static
elements as compared to 90[degrees] orientation.
[FIGURE 5 OMITTED]
F(t) curves show that the flow behaviour is a combination of that
for plug flow reactor (PFR) and stirred tank reactor (CSTR). The exact
combination of PFR and CSTR, which shows an equivalent behaviour of
static mixer, is determined by modelling. Dimensionless variance of the
residence time distribution is another common indicator of degree of
mixing. It can be calculated using:
[[sigma].sup.2] = 2 [[integral].sup.[infinity].sub.0] 1 - F(t)t dt
/ [([bar.t]).sup.2] - 1 (9)
[FIGURE 6 OMITTED]
The dimensionless variance is zero for plug flow. It is
theoretically infinite for laminar flow without diffusion, but becomes
finite in all real systems due to molecular diffusion (Nauman, 1982;
Nauman and Buffham, 1983). From the experimental data of pulse input it
is seen that the dimensionless variance for static mixer is in the range
of 0 [less than or equal to] [[sigma].sup.2] [tau] [less than or equal
to] 1. So one can formulate a two-parameter model based on the geometry
of each element (Nauman and Buffham, 1983; Li et al., 1996). It is
essentially a sub-system consisting of a stirred tank and a PFR coupled
in parallel. This sub-system behaves as a single static element. There
are N number of static elements present so the whole system is arranged
in the form of a series of sub-systems (Figure 6).
The composite density function for a system in parallel is the
weighted sum of the component density functions in both Laplace and time
domain (Nauman and Buffham, 1983). Thus for the above system of static
element (for N = 1):
[[bar.f].sub.s](s) = [phi][[bar.f].sub.c](s) + (1 - [phi])
[[bar.f].sub.p](s) (10)
where [[bar.f].sub.c](s) is the Laplace transform for stirred tank
reactor which is given by Equation (11):
[[bar.f].sub.c](s) = 1 / 1 + [tau]'s (11)
and [[bar.f].sub.p](s) is the Laplace transform for PFR which is
given by Equation (12):
[[bar.f].sub.p](s) = [e.sup.-[tau]'s] (12)
where
[tau]' = V[epsilon]/NQ = space time for subsystem (13)
The generalized formulae for N subsystems in series is given by
Equation (14):
[[bar.f].sub.s](s) = [[bar.f].sub.1](s) x [[bar.f].sub.2](s) x ...
[[bar.f].sub.N](s)) (14)
[FIGURE 7 OMITTED] But [[bar.f].sub.1](s) = [[bar.f].sub.2](s) =
... = [[bar.f].sub.N](s), so the generalized formulae in terms of
Laplace transform for proposed system is given by:
G(s) = [[[phi][[bar.f].sub.c](s) + (1 - [phi])
[[bar.f].sub.p](s)].sup.N] (15)
or
G(s) = [([phi] / 1 + ([beta]/[phi])[tau]'s + (1 - [phi]) exp
(-(1 - [beta])[tau]'s / (1 - [phi]))].sup.N] (16)
Equation (16) was converted to time domain, and simulation of the
above model for pulse input was carried out. The main advantage of this
model is that it can be applied for any type of static mixer in
practice.
The simulation results of the model are compared with the
experimental results of pulse input of tracer (NaCl) to the static mixer
system with 45[degrees] orientation of static elements. The measured
effluent concentrations were converted to dimensionless form E(t),
[t.sub.m], and [[sigma].sub.t]. The results are shown in Figures 7a
through Figure 8b, respectively. The RTD model agrees satisfactorily
with the experimental results only upto certain value of t. It does not
conform to the experimental results in which a long tail of
concentration is found with time. The values of parameters which give a
good fit are:
[phi] = 0.69 + 9.5 x [10.sup.-3] log(Re) (17)
[beta] = 0.47 (18)
CONCLUSIONS
The pressure drop results show that new static mixer gives lower
pressure drop as compared to some commercial mixers. The pressure drop
is more when the elements are oriented at 45[degrees] to each other.
This is due to increase in the number of flow paths in the axial
direction due to splitting of the primary flow. The radial flow created
by new static mixer is nearly independent of orientation of mixer
elements with respect to each other.
The cumulative distribution curves show that static mixer (MALAVIYA
mixer) with 45[degrees] orientation of static elements is more closer to
plug flow behaviour compared to 90[degrees] orientation. This is due to
more number of flow paths or more splitting of streamlines offered by
45[degrees] orientation of static elements.
The results of RTD model follow the experimental results only upto
certain range of time (t = 1.5[bar.t]), this is due to taking parameter
[beta] (fraction of total volume corresponding to CSTR) as independent
of Reynolds number and number of static elements.
ACKNOWLEDGEMENTS
The results reported in this article are based on the M.Tech.
(Chem. Eng.) dissertation of Mr Gunjan Kumar. Authors are grateful to
Prof. G. Djelveh, LGCB, Universite of Blaise Pascal, Aubiere Ledex,
France, who encouraged them to initiate work in this area.
NOMENCLATURE
A constant
b' mixing constant
[[bar.c].sub.1] average volumetric concentration of
species i (mol/L)
[c.sub.ij] volumetric concentration of species i at
sampling point j (mol/L)
[C.sub.1], [C.sub.2],
[C.sub.3] constants
[C.sub.i] initial concentration of tracer (mol/L)
[C.sub.f] final concentration of fluid (mol/L)
C(t), [C.sub.out](t) concentration of sample at time t at inlet
ends (mol/L) and outlet
C([infinity]) concentration at time t = [infinity] (mol/L)
D diameter of capillary tube (m)
[D.sub.c] diameter of static element (m)
[D.sub.e] equivalent diameter (m)
[D.sub.t] diameter of tube filled with static mixer (m)
E(t) = [C.sub.out](t)/[[integral].sup.
[infinity].sub.0] [C.sub.out] (t)dt
f Fanning friction factor with static mixing
inserts
[f.sub.empty] Fanning friction factor in an empty pipe
F(t) (C(t) - [C.sub.i])/(C([infinity]) - [C.sub.i])
K consistency index (Pa [s.sup.n])
L height of curved portion of static element
(m)
L length (m)
[L.sub.e] length of one static element (m)
m, m' constant
n flow behaviour index
N number of static elements
P pressure (N/[m.sup.2])
[DELTA][P.sub.sm] pressure drop (N/[m.sup.2])
[DELTA]P pressure difference in capillary tube
(N/[m.sup.2])
Q volumetric flow rate (L/s)
Re Reynolds number
[Re.sub.g] generalized Reynolds number
t residence time (s) [= (v / a)] (s)
[t.sub.m] mean residence time (= (V / Q)] (s)
[bar.t] dimensionless time (= t / [tau]) (s)
u superficial velocity (m/s)
v fluid velocity in capillary tube (m/s)
V volume of static mixer system ([m.sup.3])
[w.sub.d] width of disc of static element (m)
[w.sub.c] width of curved (s-shaped) part of static
element (mm)
Greek Symbols
[[??].sub.w] rate of shear at wall ([s.sup.-1])
[epsilon] static mixer system void fraction
[phi] RTD model parameter
[phi] RTD model parameter
[beta] RTD model parameter
[mu] viscosity (Pa s)
[[mu].sup.*] viscosity based on [[??].sub.w] for non-
Newtonian fluids (Pa s)
[rho] density of fluid (kg/[m.sup.3])
[[sigma].sup.2] variance ([s.sup.2])
[[sigma].sub.2 dimensionless variance [= ([[sigma].sup.2]
.sub.[tau]] / [t.sup.2.sub.m])]
[[tau].sub.w] shear stress (Pa)
[[tau].sub.s] space time (s)
Manuscript received April 18, 2007; revised manuscript received
January 14, 2008; accepted for publication January 14, 2008.
[FIGURE 8 OMITTED]
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Gunjan Kumar and S. N. Upadhyay * Department of Chemical
Engineering and Technology, Centre of Advanced Study, Institute of
Technology, Varanasi 221 005, India
* Author to whom correspondence may be addressed. E-mail addresses:
[email protected],
[email protected]
Table 1. Rheological constants and density of test fluids
1% 1.5%
[CMC.sub.hv] [CMC.sub.mv]
n 0.465 0.710
K (Pa.[s.sup.n]) 1.037 0.136
[rho] (kg/[m.sup.3]) 1007.6 1030.2
4% 10%
PVA PEC
n 0.774 0.859
K (Pa.[s.sup.n]) 0.045 0.01
[rho] (kg/[m.sup.3]) 1040 1039.2
Table 2. Constants for f-Re correlations
S. no. Reference Mixer element
1. Grace (1971) Helical
2. Sir and Lecjaks (1982), Helical
Lecjaks et al. (1984)
3. Cybulski and Helical (for Re [less
Werner (1986) than or equal to] 50)
Helical (for Re [less
than or equal to] 100,
Re [less than or
equal to] 1000)
Sulzer SMX
Sulzer SMV
Inliner Lightnin
N form
Komax
Hi-Toray
ISG
LPD
4. Shah and Kale (1991) Kenics
Sulzer
5. Chandra and Kale (1992) Komax
6. Li et al. (1997) Sulzer SMX
Re [less than or
equal to] 15
15 [less than or
equal to] Re [less
than or equal
to] 1000
Re [greater than
or equal to] 1000
7. Rauline et al. (1998) Sulzer SMX LPD
8. Cavatora et al. (1999) Sulzer S MX (20 [less
than or equal to] Re
[less than or equal
to] 1000)
9. Present work Modified disk mixer
(0[degrees]
orientation)
90[degrees] Orientation
45[degrees] Orientation
Mixer element [C.sub.1] [C.sub.2]
Helical 77.76 10.88
Helical 85.50 0.34
Helical (for Re [less 115.2 0.5
than or equal to] 50)
Helical (for Re [less 6.592
than or equal to] 100,
Re [less than or
equal to] 1000)
Sulzer SMX 160-1600
Sulzer SMV 1040-4800
Inliner Lightnin 144-118.4 11.2
N form 240-272
Komax 400
Hi-Toray 608
ISG 4000-4800
LPD 5407.5 (D/L)
Kenics 64.06n 3.68[n.sup.4]/(n + 1)
Sulzer 350n 10.26n/(n + 1)
Komax 176.5n 7.56n/(n + 1)
Sulzer SMX
Re [less than or 398
equal to] 15
15 [less than or 220
equal to] Re [less
than or equal
to] 1000
Re [greater than 12
or equal to] 1000
Sulzer SMX LPD 160-960
139.5
146.08 (D/L)
Sulzer S MX (20 [less 78.4 0.148
than or equal to] Re
[less than or equal
to] 1000)
Modified disk mixer 70 0.75
(0[degrees]
orientation)
90[degrees] Orientation 72.2 0.24
45[degrees] Orientation 88 0.24
Mixer element m a
Helical 0.5
Helical 0.0
Helical (for Re [less
than or equal to] 50)
Helical (for Re [less 0.5
than or equal to] 100,
Re [less than or
equal to] 1000)
Sulzer SMX
Sulzer SMV
Inliner Lightnin 0.0
N form
Komax
Hi-Toray
ISG
LPD
Kenics 1.36n/(n + 3)
Sulzer 2.32n/(n + 3)
Komax 1.72n/(n + 1)
Sulzer SMX
Re [less than or
equal to] 15
15 [less than or 0.8 0.8
equal to] Re [less
than or equal
to] 1000
Re [greater than 0.25
or equal to] 1000
Sulzer SMX LPD
Sulzer S MX (20 [less 0.0
than or equal to] Re
[less than or equal
to] 1000)
Modified disk mixer 0.13
(0[degrees]
orientation)
90[degrees] Orientation 0.13
45[degrees] Orientation 0.13