Turbulent flow of non-Newtonian liquids through an axisymmetric sudden expansion Rob Poole Department of Engineering, University of Liverpool Osborne Reynolds Seminar 30th April 2003 Introduction • Osborne Reynolds (1883,1895) • Newtonian flows - large literature exists • Non-Newtonian - Few previous studies [Pak et al (1990)] – Experimental: flow visualisation • Aims of this study – Use of LDA to provide quantitative data – Investigate effect on reattachment length Osborne Reynolds – Database for CFD validation Seminar 30th April 2003 Experimental rig Fully developed pipe flow d= 26 mm D=52 mm R = D2 / d2 = 4 Osborne Reynolds Seminar 30th April 2003 Working fluids • Water • Three concentrations of polyacrylamide (PAA) – 0.02%, 0.05% and 0.1% – Shear thinning to various degrees – Increasing viscoelasticity with concentration – Large extensional viscosities – Highly drag reducing – Optically transparent Osborne Reynolds Seminar 30th April 2003 Working fluids cont… N1 • Rheological data obtained – Shear viscosity vs shear rate – First normal stress difference vs shear stress Osborne Reynolds Seminar 30th April 2003 Viscosity (Pa s) Rheological data 10 2 10 1 μCY μ μ0 μ 1 ( CY 10 ) 0.02% PAA a n/a 0.05% PAA 0 0.1% PAA 10-1 10 -2 10 -3 10 -3 10 -2 10 -1 10 0 10 1 Shear rate (1/s) 10 2 10 3 Figure 2: Viscosity versus shear rate for 0.02,0.05 and 0.1% of polyacrylamide (including Carreau-Yasuda fit) 10 4 Osborne Reynolds Seminar 30th April 2003 First normal stress difference N 1 (Pa) Rheological data cont … 10 3 0.1% PAA 102 1 10 0 10 10 1 Shear stress (Pa) Figure 3: First normal stress difference N1 Osborne Reynolds Seminar 30th April 2003 versus shear stress for 0.1% PAA. 10 2 Estimation of Reynolds number • Difficulty - no single value for the viscosity characterises the fluid. • Method adopted - estimate the maximum shear rate at ‘inlet’ (x/h=1). • Example 0.02% PAA dV c dy 3000 s 1 Max Osborne Reynolds Seminar 30th April 2003 Estimation of Reynolds number • This shear rate is then used to obtain a viscosity from the Carreau-Yasuda model: μC 2.82 x10-3 Pa.s • Hence a Reynolds number of U B h U B h Re1 26000 Re2 22700 C CH Osborne Reynolds Seminar 30th April 2003 Mean axial velocity profiles 2 2 0 0 1 1 0.5 0.5 0.5 0.5 0 x/h x/h 0 rr/ /RR y/h y/h 1.5 1.5 1 1 1 1 2 2 3 3 4 4 5 5 6 6 2 0.02% PAA 1 1 Water 0 2 0 1.5 0.5 r/ R 1 1 r/ R y/h y/h 1.5 0.5 0.5 0.5 0 x/hx/h 0 1 8 9 10 12 8 9 10 12 Figure 5 (b): Mean axial velocity (U/UB) profiles Figure 5 (b): Mean axial velocity (U/UB) profiles 16 16 20 20 1 Osborne Reynolds Seminar 30th April 2003 Streamlines 1 1 y/hy/h 1 1 Water 0.5 -0.08<<0 [0.02 steps] 0<0.5 <0.35 [0.05 steps] 0.5 0.5 0 x/h 0 x/h 6 8 XR 12 2 4 Figure 7 2(a):Streamline pattern Re=30000 6 for Water 8 XR 12 4 Figure 7 (a):Streamline pattern for Water Re=30000 16 16 0.02% PAA -0.09<1 <-0.01 [0.02 steps] 0< <0.3 [0.05 steps] 1 1 1 y/hy/h 0 20 0 20 0.5 0.5 0.5 0 x/h 0 x/h 0.5 2 4 6 8 10 12 Figure 7 2(b):Streamline pattern PAA 4 6 for 0.02% 8 10 Re=26000 12 Figure 7 (b):Streamline pattern for 0.02% PAA Re=26000 16 16 Osborne Reynolds 0 Seminar X 0 30th April 2003 X R R Axial Reynolds stresses (u) 22 00 0.25 0.25 y/h r/ R r/ R 1.5 1.5 11 0.5 0.5 0.5 0.5 x/h x/h 00 11 22 33 44 55 11 66 22 0.02% PAA Water 00 y/h R rr // R 1.5 1.5 11 0.5 0.5 0.5 0.5 00 x/h x/h 88 99 10 12 10 12 Figure 10 (b): Axial turbulence intensity (u' /U Figure 10 (b): Axial turbulence intensity (u' /UB)B)profiles profiles 16 16 2020 11 Osborne Reynolds Seminar 30th April 2003 Radial Reynolds stresses (v) 22 0.25 0.25 00 11 0.5 0.5 rr/ /RR y/h y/h 1.5 1.5 0.5 0.5 0 x/h x/h 0 22 1 1 2 2 3 3 4 4 5 5 6 6 0.02% PAA 11 00 Water 11 0.5 0.5 rr/ /RR y/h y/h 1.5 1.5 0.5 0.5 00 x/h x/h 88 99 10 12 10 12 Figure 12 (b): Radial turbulence intensity (v' /U profiles Figure 12 (b): Radial turbulence intensity (v' /UB)) profiles B 16 16 20 20 11 Osborne Reynolds Seminar 30th April 2003 Mean axial velocity profiles 4 3.5 3 3 y/h No recirculation 2.5 0.1% PAA Re 4000 XR32 2 1.5 1 1 1 0.5 0 x/h 1 3 6 12 Figure 9 (a): Mean axial velocity (U/UB) profiles for 0.1% PAA Re= 4000 Osborne Reynolds Seminar 30th April 2003 Concluding remarks • Turbulent flow through an axisymmetric sudden expansion of area expansion ratio (i.e. D2/d2) 4. • Water and two lowest conc. of PAA - axisymmetric. • Reattachment lengths were Water XR 10 step heights 0.02% and 0.05% PAA XR 20 step heights Osborne Reynolds Seminar 30th April 2003 Concluding remarks cont… • Increase in XR caused by modifications to turbulence structure with large reductions in v and w resulting in reduced transverse transfer of axial momentum. • At highest conc. of PAA axisymmetric flow could not be achieved. This could be due to an elastic instability or a slight geometric imperfection that is accentuated by viscoelasticity. Osborne Reynolds Seminar 30th April 2003