BAIL 2006 Book of Abstracts - Institut für Numerische und ...

BAIL 2006 Book of Abstracts - Institut für Numerische und ... BAIL 2006 Book of Abstracts - Institut für Numerische und ...

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A. NAYAK, D. DAS: Three-dimesnional Temporal Instability of Unsteady Pipe Flow ✬ ✫ 2 >2 R=1 (at wall) R=0 (center-line) R=1 (at wall) R=0 (center-line) R=1 (at wall) u = 0 v = 0 u ′ = 0 u = 0 v = 0 u ′ + iv′ = 0 3 u ′′ + 2iv ′′ = 0 u = 0 v = 0 u ′ = 0 u = 0 v = 0 u ′ = 0 v ′ = 0 u = 0 v = 0 u ′ = 0 Table. 1 Boundary conditions for perturbation at wall and the centerline For n=0, the two equations decouple to give a fourth order equation in u and a second order n−1 equation in v . For n=1, the seventh condition is u ∝ r when limr → 0 (Batchelor & Gill 1962). 4.4 Results and Discussions We have considered a case (case2 of Das & Arakeri 1998) in which a perceptible wave was observed through flow visualization at time t= t . During this period the piston has stopped after a p ( 2 trapezoidal motion and the profile considered for analysis is at time 1 t t2 t p t 4 − + = ) where, t2 is the time when piston has stopped. The neutral stability curves are shown in figure 1. It is observed that critical Reynolds number for n=1 mode is minimum (=398). Figure 2 shows the corresponding flow visualization picture of Das & Arakeri (1998). The position of vortex wave at 0 90 phases between top and bottom portion of pipe is visible in figure 2. Hence the helical mode with n=1 is most unstable in this case. As the neutral curve for n=0 mode is close to n=1 mode for some cases n=0 mode might be most unstable mode. Symmetric modes has been observed as most unstable in other cases experimentally (Das & Arakeri 1998 case 3 ). The stability analysis will be shown in the final paper for these cases, but the neutral curves (figure1) itself indicate the possibility of growth of such axisymmetric modes. The calculated wave length is λ ≈ 3. 22 δ matches with the wavelength observed in experiment, the value of which is approximately 3.0. alpha (α) 8 7 6 5 4 3 2 Neutral Stability Curve for n 0, 1 & 2 n=0 n=1 n=2 1 200 300 400 500 600 700 800 900 1000 1100 1200 Reynolds number (Re) Fig.1 Neutral Stability Curve for different n Fig. 2 Flow viz. picture of Das & Arakeri (case2) REFERENCES 1. Batchelor, G. K. & Gill, A. E. 1962. J. Fluid Mech. 14, 529. 2. Das, D. 1998 Ph.D Thesis, Department of Mechanical Engg, Indian Institute of Science, Bangalore. 3. Das, D. & Arakeri, J. H. 1998. J. Fluid Mech. 374, 251-283. 4. Das, D. & Arakeri, J. H. 2000 Unsteady Jl. Applied Mech. 67, 274-281. 5. Nayak, A. 2005 MTech report Dept of Aerospace Engg, Indian Institute of Technology, Kanpur. 6. Uchida, S. 1956 Z. Angrew. Math. Phys. 7, 403-422. 7. Weinbaum, S. & Parker, K. 1975. J. Fluid Mech. 69, 729-752. Speaker: DAS, D. 36 BAIL 2006 ✩ ✪

J. HUSSONG, N. BLEIER, V.V. RAM: The structure of the critical layer of a swirling annular flow in transition ✬ ✫ The structure of the critical layer of a swirling annular flow in transition J. Hussong, N. Bleier and V. Vasanta Ram Ruhr-Universität Bochum, D-44780 Bochum, Germany Subject of our paper falls under the heading of transition of the swirling flow in an annulus. Two transition mechanisms with some fundamental differences, which we call the Taylor and the Tollmien-Schlichting mechanisms, are generally in competition with each other in this flow. The salient difference referred to is the presence of a critical layer in the Tollmien-Schlichting mechanism. In contrast, such a critical layer is absent in the Taylor mechanism. The focus of attention in our work is the modification swirl causes to the structure of this critical layer in annular flow. The characteristic feature of the critical layer is that the propagation velocity of the disturbance wave is the same as the local velocity in the basic flow. Mathematically, this results in the equations for the propagation of small amplitude disturbances exhibiting a turning point, i.e. the coefficient of a crucial term in the governing differential equations crossing a zero value (see eg. [5], [6], [2], [3], [7]). For this reason viscous effects gain importance in the critical layer which may be regarded as an internal layer in the flow. The viscous effects have to be taken properly into account in the critical layer in order to arrive at the stability characteristics of the flow of interest undergoing transition. Our basic flow is the fully developed flow with swirl in the uniform annular gap between concentric circular cylinders. In the flow in this geometrical configuration, swirl comes into existence when the axial pressure gradient driving the flow acts in conjunction with a rotation of a cylinder about its own axis. We restrict our attention for the present to the case when the outer cylinder is set in rotation at an angular velocity Ωa and the inner cylinder is pulled axially at a translational velocity Vwi. Both of these flow boundary conditions tend to raise the critical Reynolds number of the flow. The geometrical and flow pa- rameters in our problem are, in a self-explanatory notation: the transverse curvature parameter ɛR = Ra−Ri Uref x (Ra−Ri) , the Reynolds number Re = Ra+Ri 2 ν with Uref x = (Ra−Ri)2 � � � dPG Uref �, ϕ 8µ dx the swirl parameter Sa = Uref x with Uref ϕ = ΩaRa and the translational wall velocity parameter Twi = Vwi Uref x . We have approached the transition problem in this flow configuration by conducting a modal analysis of the dynamics of the propagation of disturbances in the basic flow in question, starting from small amplitude disturbances for which the governing equations may be linearised. The dispersion relationship for this linearized problem may formally be written as F(ɛR, Re, Sa, Twi, λx, nϕ, ω) = 0, Speaker: RAM, V.V. 37 BAIL 2006 ✩ ✪

J. HUSSONG, N. BLEIER, V.V. RAM: The structure <strong>of</strong> the critical layer <strong>of</strong> a swirling<br />

annular flow in transition<br />

✬<br />

✫<br />

The structure <strong>of</strong> the critical layer <strong>of</strong> a swirling annular<br />

flow in transition<br />

J. Hussong, N. Bleier and V. Vasanta Ram<br />

Ruhr-Universität Bochum, D-44780 Bochum, Germany<br />

Subject <strong>of</strong> our paper falls <strong>und</strong>er the heading <strong>of</strong> transition <strong>of</strong> the swirling flow<br />

in an annulus. Two transition mechanisms with some f<strong>und</strong>amental differences,<br />

which we call the Taylor and the Tollmien-Schlichting mechanisms, are generally<br />

in competition with each other in this flow. The salient difference referred to<br />

is the presence <strong>of</strong> a critical layer in the Tollmien-Schlichting mechanism. In<br />

contrast, such a critical layer is absent in the Taylor mechanism. The focus <strong>of</strong><br />

attention in our work is the modification swirl causes to the structure <strong>of</strong> this<br />

critical layer in annular flow.<br />

The characteristic feature <strong>of</strong> the critical layer is that the propagation velocity<br />

<strong>of</strong> the disturbance wave is the same as the local velocity in the basic flow.<br />

Mathematically, this results in the equations for the propagation <strong>of</strong> small amplitude<br />

disturbances exhibiting a turning point, i.e. the coefficient <strong>of</strong> a crucial<br />

term in the governing differential equations crossing a zero value (see eg. [5],<br />

[6], [2], [3], [7]). For this reason viscous effects gain importance in the critical<br />

layer which may be regarded as an internal layer in the flow. The viscous effects<br />

have to be taken properly into account in the critical layer in order to arrive at<br />

the stability characteristics <strong>of</strong> the flow <strong>of</strong> interest <strong>und</strong>ergoing transition.<br />

Our basic flow is the fully developed flow with swirl in the uniform annular<br />

gap between concentric circular cylinders. In the flow in this geometrical configuration,<br />

swirl comes into existence when the axial pressure gradient driving<br />

the flow acts in conjunction with a rotation <strong>of</strong> a cylinder about its own axis.<br />

We restrict our attention for the present to the case when the outer cylinder is<br />

set in rotation at an angular velocity Ωa and the inner cylinder is pulled axially<br />

at a translational velocity Vwi. Both <strong>of</strong> these flow bo<strong>und</strong>ary conditions tend to<br />

raise the critical Reynolds number <strong>of</strong> the flow. The geometrical and flow pa-<br />

rameters in our problem are, in a self-explanatory notation: the transverse curvature<br />

parameter ɛR = Ra−Ri<br />

Uref x (Ra−Ri)<br />

, the Reynolds number Re = Ra+Ri 2 ν with<br />

Uref x = (Ra−Ri)2 � �<br />

� dPG<br />

Uref �,<br />

ϕ<br />

8µ dx the swirl parameter Sa = Uref x with Uref ϕ = ΩaRa and<br />

the translational wall velocity parameter Twi = Vwi<br />

Uref x .<br />

We have approached the transition problem in this flow configuration by<br />

conducting a modal analysis <strong>of</strong> the dynamics <strong>of</strong> the propagation <strong>of</strong> disturbances<br />

in the basic flow in question, starting from small amplitude disturbances for<br />

which the governing equations may be linearised. The dispersion relationship<br />

for this linearized problem may formally be written as<br />

F(ɛR, Re, Sa, Twi, λx, nϕ, ω) = 0,<br />

Speaker: RAM, V.V. 37 <strong>BAIL</strong> <strong>2006</strong><br />

✩<br />

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