Term Project I

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    T.C. Baheehir University

    03.28.2011

    Term Project IIntroduction to CFD

    0678821 Burak SUNAN

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    TERM PROJECT I

    LAMINAR FLOW IN A CHANNEL AND PIPE

    Introduction

    The object of the project is to obtain a CFD solution for the laminar flow in a channel and a pipe

    by using above parameters with FLUENT.

    Vm (m/s) D (m) L (m) Re M N

    1 1,6 120 800 80 40

    Vm: Velocity inlet

    D: Planar Height (Pipe Diameter)

    L: Planar (Pipe) Length

    Re: Reynolds Number

    M: row number of mesh

    N: Column number of mesh

    Laminar Channel Flow Calculation

    The geometry and mesh are created in ANSYS 12.1 which is the preprocessor for FLUENT, and

    the mesh is read into FLUENT and solved for the flow solution.

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    Firstly, the analysis type is changed to 2D from 3D in order to solve channel and pipe flows from

    Properties part before beginning to process geometry for a channel flow from FLUENT.

    Secondly, the channel flow is drawn from geometry part. In details view, H1 is entered the flow

    length 120 m and V2 is entered the flow height is 1.6 m.

    Thirdly, the mesh is mapped with 80 rows and 40 columns from edge sizing parts and then the

    channel flow is named as wall, symmetry, velocity inlet, and pressure outlet.

    Fourthly, flow calculation data are initiated in setup section with double precision. Planar below

    2D space from general part, is selected in order to specify a channel flow. Laminar is obtained

    from models as a viscous model. In materials part, the air density and viscosity values are

    changed to 1 kg/m3 and 0.002 kg/m-s. In the boundary conditions part, the velocity inlet

    magnitude is specified 1 m/s and the other zones (pressure outlet, wall and symmetry) are

    checked if they have right match. Therefore, calculation is run after all data entrances.

    Laminar Channel Flow Results

    Figure 1. Contour plots of X velocity

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    Figure 2. Contour plots of pressure

    Figure 3. XY plots of X versus X velocity along the centerline

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    Figure 4. XY plots of Xvelocity versus Y at the pressure outlet

    Figure 5. XY plots of pressure versus X along the centerline

    Table 1. Drag force acting on the body

    Forces Pressure

    Zone Wall (0 25.032583 0)

    Net (0 25.032583 0)

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    Laminar Pipe Flow Calculation

    In order to calculate the pipe flow, there is an easy way that duplicates the channel flow part

    from FLUENT. Mainly, most of processes are same with the channel flow.

    Firstly, Axisymmetric is chosen instead of planar in 2D Space part of Setup section. Rests of all

    processes from geometry to contour results are same with the channel flow.

    Laminar Pipe Flow Results

    Figure 6.Contour plots of X velocity

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    Figure 7.Contour plots of pressure

    Figure 8.XY plots of X versus X velocity along the centerline

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    Figure 9.XY plots of Xvelocity versus Y at the pressure outlet

    Figure 10.XY plots of pressure versus X along the centerline

    Table 2.Drag force acting on the body

    Forces Pressure

    Pipewall (-7.0948164e-14 0 0)

    Net (-7.0948164e-14 0 0)

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    Conclusion

    Figure 11. Comparison_XY plots of Xvelocity versus Y at the pressure outlet

    Figure 12. Comparison_XY plots of pressure versus X along the centerline

    Above the figures, the dark lines show the pipe flow and white lines show the channel flow.

    Therefore, we can easily see the pressure differences at the outlet and along the centerline

    between the pipe and channel flows.