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Three-dimensional stability of the flow past a rotating cylinder Jan - PowerPoint PPT Presentation

Three-dimensional stability of the flow past a rotating cylinder Jan O. Pralits 1 , F. Giannetti 2 1Department of Chemical, Civil and Environmental Engineering University of Genoa, Italy jan.pralits@unige.it 2Department of Industrial Engineering


  1. Three-dimensional stability of the flow past a rotating cylinder Jan O. Pralits 1 , F. Giannetti 2 1Department of Chemical, Civil and Environmental Engineering University of Genoa, Italy jan.pralits@unige.it 2Department of Industrial Engineering University of Salerno, Italy fgiannetti@unisa.it September 10, 2012 The work has been carried out in collaboration with: Luca Brandt KTH, Stockholm, Sweden; EFMC9 - September 10 th 2012 - Roma (Italy) Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 1 / 18

  2. Background Problem formulation Incompressible flow y U * Re = U ∗ D ∗ ν ∗ Ω * x α = Ω ∗ D ∗ D * 2 U ∗ � ∞ 1 U ( x , y , z , t ) = U b ( x , y ) + ǫ √ u ( x , y , κ ) exp( i κ z + σ t ) d κ 2 π −∞ Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 2 / 18

  3. Background Steady flow ¡ Vorticity field at Re = 100 and (a) α = 1 . 8, (b) α = 4 . 85. ¡ Force in cross-stream direction Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 3 / 18

  4. Background Neutral curve Two-dimensional perturbations ( κ = 0) 7 6 Mode II 5 4 α 3 2 1 Mode I 0 0 50 100 150 200 Re Previous studies Pralits et al. (2010), Stojkovic et al. (2002), Mittal (2003), Kang et al. (1999) Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 4 / 18

  5. Background Shedding mode I & II ¡ ¡ ¡ ¡ ¡ ¡ ¡ ¡ ¡ ¡ ¡ ¡ ¡ ¡ ¡ ¡ ¡ Re = 100, Vorticity field (a) α = 1 . 8, (c) α = 4 . 85, Adjoint field (b) α = 1 . 8, (d) α = 4 . 85 Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 5 / 18

  6. Motivation for further studies Motivation Missing bits... Shedding mode II (2D) has not been verified in experiments (ex. Yildirim et al.) 3D effects might be important Main goal Determine if 3D effects are important Draw a neutral curve accounting for 3D instabilities Determine critical conditions Bifurcation diagram at branch II Sensitivity analysis Experiments: Yildirim et al. EFMC 7 Compare with experiments by Linh (2011) Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 6 / 18

  7. Stability analysis 3D Shedding mode II α =5 α =5 α =4.75 α =4.75 0.15 0.25 0.1 0.2 0.05 0.15 σ r σ i 0.1 0 −0.05 0.05 −0.1 0 −0.05 0 1 2 3 4 5 0 1 2 3 4 5 κ κ Growth rate σ r (left) and Strouhal number St = σ i / (2 π ) (right) for Re = 100 as a function of the rotation rate and spanwise wave number. Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 7 / 18

  8. Stability analysis 3D Shedding mode II α =5 α =5 α =4.75 α =4.75 0.15 0.25 0.1 0.2 0.05 0.15 σ r σ i 0.1 0 −0.05 0.05 −0.1 0 −0.05 0 1 2 3 4 5 0 1 2 3 4 5 κ κ Growth rate σ r (left) and Strouhal number St = σ i / (2 π ) (right) for Re = 100 as a function of the rotation rate and spanwise wave number. A new stationary three-dimensional mode II is found... Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 7 / 18

  9. Stability analysis 3D Shedding mode II α =5 α =5 α =4.75 α =4.75 0.15 0.25 0.1 0.2 0.05 0.15 σ r σ i 0.1 0 −0.05 0.05 −0.1 0 −0.05 0 1 2 3 4 5 0 1 2 3 4 5 κ κ Growth rate σ r (left) and Strouhal number St = σ i / (2 π ) (right) for Re = 100 as a function of the rotation rate and spanwise wave number. A new stationary three-dimensional mode II is found... ...with approximately 3 times the growth rate of the 2D unsteady one. Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 7 / 18

  10. Stability analysis 3D Shedding mode I & II σ r ( α, κ ) ≥ 0 Re = 40 (left) and Re = 50 (right) 6 6 5 5 4 4 α 3 α 3 2 2 1 1 0 0 −6 −4 −2 0 2 4 6 −6 −4 −2 0 2 4 6 κ κ Re = 60 (left) and Re = 100 (right) 6 6 5 5 4 4 α 3 α 3 2 2 1 1 0 0 −6 −4 −2 0 2 4 6 −6 −4 −2 0 2 4 6 κ κ Contours: 0, 0.02, 0.04, 0.06, 0.08, 0.1, 0.12 Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 8 / 18

  11. Stability analysis 3D Neutral curve 7 2D 3D 6 5 4 Mode II α 3 2 1 Mode I 0 0 50 100 150 200 Re Neutral stability curve of two and three-dimensional perturbations. Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 9 / 18

  12. Stability analysis 3D Neutral curve 7 2D 3D 6 5 4 Mode II α 3 2 1 Mode I 0 0 50 100 150 200 Re Neutral stability curve of two and three-dimensional perturbations. Critical condition: Re c ≈ 33, α c ≈ 5 . 8 Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 9 / 18

  13. Stability analysis 3D Neutral curve 7 2D 3D 6 5 4 Mode II α 3 2 1 Mode I 0 0 50 100 150 200 Re Neutral stability curve of two and three-dimensional perturbations. Critical condition: Re c ≈ 33, α c ≈ 5 . 8 A pitchfork bifurcation occurs at critical conditions and the instability is 3D Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 9 / 18

  14. Stability analysis 3D Experiments by Linh, PhD thesis, NUS, 2011 ... spent more than 10 times the duration to capture the regular vortex shedding in order to wait for that vortex to appear again, but no regular one-sided vortex shedding could be detected. It might be due to the three dimensional disturbances of the current experimental flow because of the finite cylinder length and differences in cylinder end conditions. To the best of the authors knowledge, there is no published three dimensional numerical study to confirm the existence of such instability in 3-D flow. Thus it is reasonable to speculate that the second instability is a two-dimensional flow phenomenon with evidences gathered so far. From Linh (2011) Re = 206, α = 4 λ ≈ 1 . 25 D − 1 . 5 D → κ ≈ 5 − 4 . 2 0.3 0.25 0.2 0.15 σ r 0.1 0.05 0 −0.05 −0.1 0 2 4 6 8 10 12 κ ¡ Vorticity (PIV) Linear stability analysis , σ i = 0 Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 10 / 18

  15. Stability analysis 3D Shedding mode II comparison: # I Absolute value of the perturbation vorticity field for Re = 100, α = 5 4 4 3 3 2 2 1 1 0 0 −1 −1 −2 −2 −2 −1 0 1 2 3 4 5 6 −2 −1 0 1 2 3 4 5 6 κ = 0 κ = 1 max | ω ( x , y , κ = 1) | / max | ω ( x , y , κ = 0) | ≈ 2. The white curve shows the stagnation line. Note that for κ = 1 the vorticity is aligned with maximum strain. Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 11 / 18

  16. Stability analysis 3D Shedding mode II comparison: # II Absolute value of the adjoint velocity field for Re = 100, α = 5 7 7 6 6 5 5 4 4 3 3 2 2 1 1 0 0 −1 −1 −2 −2 −10 −8 −6 −4 −2 0 2 −10 −8 −6 −4 −2 0 2 κ = 0 κ = 1 max | u ⋆ ( x , y , κ = 1) | / max | u ⋆ ( x , y , κ = 0) | ≈ 2. The white curve shows the stagnation line. Note that for κ = 1 the vorticity is aligned with compression Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 12 / 18

  17. Stability analysis 3D Shedding mode II comparison: # III Structural sensitivity for Re = 100, α = 5 S p ( x 0 , y 0 ) = u ⋆ ( x 0 , y 0 ) u ( x 0 , y 0 ) 4 4 , � 3 3 u ⋆ · u dS 2 2 Ω 1 1 max � S p ( κ = 1) � ≈ 3 0 0 max � S p ( κ = 0) � −1 −1 −2 −2 −2 −1 0 1 2 3 4 5 6 −2 −1 0 1 2 3 4 5 6 4 4 3 3 S b ( x 0 , y 0 ) = U ⋆ b ( x 0 , y 0 ) U b ( x 0 , y 0 ) , 2 2 � u ⋆ · u dS 1 1 Ω 0 0 max � S b ( κ = 1) � ≈ 7 −1 −1 max � S b ( κ = 0) � −2 −2 −2 −1 0 1 2 3 4 5 6 −2 −1 0 1 2 3 4 5 6 κ = 0 κ = 1 Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 13 / 18

  18. Conclusions Conclusions A new stationary three-dimensional mode II is found... ...with approximately 3 times the growth rate of the 2D unsteady one. A neutral curve has been shown in the plane ( α, Re ) which accounts for 3D perturbations Critical condition: Re c ≈ 33 , α c ≈ 5 . 8 (below classical Von Karman) A pitchfork bifurcation occurs at critical conditions and the instability is 3D The bifurcation at branch II of mode II is approximately 2D (as in Pralits et al., 2010) Flow is linearly stable for 3D disturbances when α > 2 nd turning point (as in 2D) LST predicts the steady 3D mode observed in experiments by Linh (2011) at Re = 206 Need ” real ” 2D experiment, eg. SOAP FILM, to reproduce the non-stationary mode II Is the stationary 3D mode II an hyperbolic instability ? (stationary, aligned with direction of maximum strain, 3D, situated on a hyperbolic stagnation point.) Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 14 / 18

  19. Conclusions Extra slides Pralits, Giannetti (UNIGE,UNISA) 3D stability of rotating cylinder September 10, 2012 15 / 18

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