My BTech thesis involved the modeling of air-flow in a passageway. One of its walls is covered with a dense tropical creeper. Since we planned to use a wall-function-invoked SST k-omega turbulence model, the boundary layer thickness needed to be calculated. This was done as follows:

  • Since the wall is not a continuous surface (dense, porous foliage), the boundary layer on the wall would intermittently be sucked in by the creeper
  • Therefore, we can assume the boundary layer to be reformed after successive space intervals. This interval was taken to be half the length at which transition to turbulence would occur, i.e. 3.5 m
  • Based on this length, the maximum boundary layer thickness is calculated to be 11.24 cm.
  • The actual geometry did not explicitly model the foliage (i.e., the wall was a simple smooth wall). When wall-functions are being used, the first layer thickness of the mesh must be greater than the maximum boundary layer thickness. We chose a first layer thickness of 13 cm, which corresponded to a y-plus value of 15.This also ensured that the boundary layer was forced to stay under 13 cm even for the smooth wall in the numerical model. We understand that 15 is very close to the minimum allowed y-plus value of 11 for wall-function models.

    My question is, is this the right approach to tackling this problem? Are there better ways of modeling this? Please find the paper attached for reference.

    Thank you for your response.

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