Abstract
The turbulent flow of mildly elastic drag reducing fluids through a straight tube rotating around an axis perpendicular to its own is analysed using boundary layer approximations. The momentum integral approach is used and the governing equations have been solved numerically using the Runge-Kutta-Merson method. The influence of the Deborah number on the velocity distribution and the boundary layer thickness has been exemplified through the analysis.
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Abbreviations
- a :
-
radius of the rotating tube
- A, B :
-
constant in equation (12)
- C :
-
pressure gradient in z-direction, −∂p*/∂z as given by equation (21)
- D :
-
characteristic angular velocity component in equation (38)
- D 0 :
-
dimensionless value of D as given by equation (48)
- D 1 :
-
angular velocity component defined by equation (63)
- D 3 :
-
coefficient in equation (63)
- De:
-
Deborah number (\(\left( {\frac{{\theta _1 u^{*2} }}{v}} \right)\))
- f :
-
friction factor for turbulent flow in stationary straight tubes
- f rt :
-
friction factor for rotating tubes given by equation (61)
- f 1, f 2, f 3, f 4, f 5 :
-
functions defined by equations (52)–(56)
- F(x):
-
arbitrary function of x defined by equation (11)
- p :
-
pressure appearing in equation (4)
- p*:
-
pressure in rotating system defined by equation (4)
- r :
-
distance in the radial direction
- Re:
-
Reynolds number defined by equation (28)
- u :
-
radial velocity component
- u*:
-
friction velocity (\(\left( { = \sqrt {\frac{{\tau _w }}{\rho }} } \right)\))
- U :
-
velocity component in the x-direction
- U 1 :
-
velocity scale near pipe wall as given by equation (40)
- v :
-
axial velocity component
- V :
-
velocity component in the y-direction
- w :
-
velocity component in the z-direction
- w 0 :
-
dimensionless value of w 1 given by equation (49)
- w 1 :
-
axial velocity component at the edge of the boundary layer
- w m :
-
value of the W at the centre of the tube
- W :
-
velocity component in the z-direction
- x, y, z :
-
three directions of the co-ordinate system
- α, β :
-
functions of De for dilute drag reducing fluids, respectively appearing in equation (36)
- α*:
-
integral defined by equation (59)
- δ :
-
boundary layer thickness
- δ :
-
dimensionless boundary layer thickness defined by equation (47)
- δ 1 :
-
dimensionless boundary layer thickness defined by equation (62)
- δ 2 :
-
coefficient in equation (62)
- θ :
-
angular co-ordinate
- θ 1 :
-
fluid relaxation time
- μ :
-
viscosity of a drag reducing fluid/Newtonian fluid
- ν :
-
kinematic viscosity
- ξ :
-
radial distance from the wall (=a−r)
- ρ :
-
density of the fluid
- τ w :
-
wall shear stress
- τ rθ , τ rz :
-
shear stress components defined by equations (34) and (35) respectively
- ψ :
-
shear function defined in equation (10)
- Ω:
-
angular velocity
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NCL Communication No. 3354.
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Shenoy, A.V. Turbulent flow of mildly elastic fluids through rotating straight circular tubes. Appl. Sci. Res. 43, 39–54 (1986). https://doi.org/10.1007/BF00385727
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DOI: https://doi.org/10.1007/BF00385727