Baines Reference

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    CFD-Reference: Tall building in a boundary-layer

    velocity field

    As reference example for the application of the CFD module of PHYSICA in the field of

    building aerodynamics the pressure distributions over the sidees and the top of a tall

    building model have been computed. The obtained results are then compared to the

    experimental results of:

    [1] W.D. Baines:Effects of Velocity Distribution on Wind Loads and Flow Patterns on

    Buildings. Proceedings of Symposium No. 16: Wind Effects on Buildings and Structures,

    held at the National Physical Laboratory, England, 1963. Published by HMSO London1965.

    which can be found together with other experimental results in the field of bluff-body

    aerodynamics in:

    [2] E. Simiu, R. Scanlan:Wind Effects On Structures. Third Edition, John Wiley and

    Sons. 1996. Pp. 164-165

    Geometrical Parameters

    The fluid domain was discretized using an automatic tetrahedra netgenerator. Further modelconfigurations are listed in a table given below.

    Model configuration v.1 v.2 v.3

    Height of building 160.0m

    Side length 19.72m

    Height/ Side ratio 8.1143

    Total length of

    domain (in-flow dir.)

    1000.0m

    Total width (cross-

    flow dir.)

    600.0m

    Total height () 600.0m

    Upstream length (luff

    side of building)

    200.0m

    Blocking ratio 0.88%

    Finite volumes 90373

    CFD-Reference: W.D. Baines tall building 1/6

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    CFD-Reference: W.D. Baines tall building 2/6

    Figure 1: Fluid domain (90373 tetrahedral volumes), detail building (below)

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    Inflow condition, turbulence parameters

    The inflow condition was set to a boundary layer wind profile using SOFiLOAD:

    WINDLOADING

    Wind according to code DIN 1055-4 (2004) Zone 2 Terrain category Regelprofil Binnenland

    atmospheric wind v = 64.02 [m/sec]

    Mean reference wind speed vref = 25.00 [m/sec]

    Wind direction 1.000 0.000 0.000

    Reference point 0.000 0.000 0.000 [m]

    Reference direction 0.000 1.000 0.000

    Surface height 0.000 [m]

    - Coefficients o(Karman) A1 A2 A3 B1 B2 C coherences

    Longitudinal 4.000 0.000 0.000 0.000 70.800 0.833 0.221 0.110 0.110

    Lateral 4.000 0.000 3021.00 0.000 283.200 1.833 0.114 0.167 0.167

    Vertical 4.000 0.000 3021.00 0.000 283.200 1.833 0.114 0.167 0.167

    Windprofiles (according to design code or explicit specification)

    h v-mean v-boe t-lon t-lat t-ver l-lon l-lat l-ver phase

    [m] [m/sec] [m/sec] [m/sec] [m/sec] [m/sec] [m] [m] [m] [-]

    8.000 20.33 31.43 4.73 0.00 0.00 79.986 0.000 0.000 0.000

    82.000 35.01 46.66 4.75 0.00 0.00 206.216 0.000 0.000 0.000157.000 38.84 50.44 4.75 0.00 0.00 251.743 0.000 0.000 0.000

    231.000 41.32 52.84 4.75 0.00 0.00 280.249 0.000 0.000 0.000

    305.000 43.19 54.63 4.75 0.00 0.00 301.259 0.000 0.000 0.000

    379.000 44.72 56.07 4.75 0.00 0.00 317.904 0.000 0.000 0.000

    454.000 46.03 57.30 4.75 0.00 0.00 331.851 0.000 0.000 0.000

    528.000 47.16 58.35 4.75 0.00 0.00 343.573 0.000 0.000 0.000

    602.000 48.16 59.27 4.75 0.00 0.00 353.784 0.000 0.000 0.000

    The pressure distribution of the reference solution is given as pressure coefficients, i.e.

    pressure divided by the stagnation pressure:

    So here we use the following constants:

    vref = 38.96 m/s (Reference velocity on highest point of building)

    = 1.25 kg/m (Reference density of air)

    CFD-Reference: W.D. Baines tall building 3/6

    cp=p

    1

    2v ref

    2

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    The turbulence parameters for the k- standard model where identified with a turbulence

    intensity T = 10 % and a length scale of Lt = 20m (side length of building) according:

    to:

    k = 7.70 m/s (variance of velocity)

    = 1.25 m/s (eddy energy dissipation)

    CFD-Reference: W.D. Baines tall building 4/6

    k=1

    2T v ref

    2

    =k

    3

    2

    Lt

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    CFD-Reference: W.D. Baines tall building 5/6

    Figure 3: Reference solution [2]

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    CFD-Reference: W.D. Baines tall building 6/6

    Figure 4: CFD solution (model configuration v.1)