Velocity statistics for rough-wall turbulent boundary layer flow over LEGO roughness elements in different layouts
Velocity statistics for rough-wall turbulent boundary layer flow over LEGO roughness elements in different layouts
This dataset presents 2D PIV experimental data collected over a range of twelve urban roughnesses with different frontal and plan solidities. These are described in:
[1] Placidi, M., & Ganapathisubramani, B. (2015). Effects of frontal and plan solidities on aerodynamic parameters and the roughness sublayer in turbulent boundary layers. Journal of Fluid Mechanics, 782, 541–566. http://doi.org/10.1017/jfm.2015.552
[2] Placidi, M., & Ganapathisubramani, B. (2018). Turbulent Flow Over Large Roughness Elements: Effect of Frontal and Plan Solidity on Turbulence Statistics and Structure. Boundary-Layer Meteorology, 167, 99–121. http://doi.org/10.1007/s10546-017-0317-3
[3] 3] Placidi M. & Ganapathisubramani, B (2019). Velocity statistics for rough-wall turbulent boundary layer flow over LEGO roughness elements in different layouts. DOI: 10.5258/SOTON/D0829.
PLEASE CITE THESE PAPERS AND THIS DATASET DOI WHEN USING THE DATA.
Contact Dr Marco Placidi (m.placidi@surrey.ac.uk) or Prof Bharathram Ganapathisubramani (G.Bharath@soton.ac.uk) for any queries on the dataset.
$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$
Format of the dataset:
d = Virtual origin [mm]
delta = Boundary layer thickness (delta99 [mm])
deltas = Displacement thickness [mm]
dyn_visc_air = Air dynamic viscosity [Kg/(m s)]
h = Height of the roughness [mm]
K = Acceleration parameter as in [1]
rho_air = Air density [kq/m^3]
run = Case ID as in [1] and [2]
theta = Momentum thickness [mm]
U = Mean streamwise velocity [m/s]
U_edge = Mean streamwise velocity at the edge of the boundary layer [m/s]
utau = Skin friction velocity [m/s] based on drag measurements
uu = Streamwise velocity fluctuations
uv = Reynolds shear stresses
V = Mean wall-normal velocity [m/s]
vv = Wall-normal velocity fluctuations
X = Streamwise coordinate [mm]
Y = Wall-normal coordinate [mm]
y0 = Roughness length [mm]
Additional notes on the dataset:
- The 2D PIV dataset has been averaged across the Field of View in the streamwise direction to obtain 1D profiles.
- utau is measured directly by means of a floating-element drag balance as described in [1].
- y0,d, are obtained via best fitting the velocity profiles as in [1].
- The entire dataset has been filtered to match the local resolution for all cases, as discussed in [1].
- The acceleration parameter is defined in [1], and it is calculated from 2D PIV data across the size of the drag balance sensing element (i.e. 200 mm x200 mm). As such, it is affected by a significant experimental uncertainty. Additional verification of ZPG conditions were obtained via Pitot tube measurements between the inlet and outlet of the tunnel test section. The pressure gradient was considered negligible.
Rough-wall boundary layer, LEGO roughness
University of Southampton
Placidi, M.
7c8407cd-0652-4e34-add4-b23cc73ede66
Ganapathisubramani, Bharathram
5e69099f-2f39-4fdd-8a85-3ac906827052
Placidi, M.
7c8407cd-0652-4e34-add4-b23cc73ede66
Ganapathisubramani, Bharathram
5e69099f-2f39-4fdd-8a85-3ac906827052
Placidi, M. and Ganapathisubramani, Bharathram
(2019)
Velocity statistics for rough-wall turbulent boundary layer flow over LEGO roughness elements in different layouts.
University of Southampton
doi:10.5258/SOTON/D0829
[Dataset]
Abstract
This dataset presents 2D PIV experimental data collected over a range of twelve urban roughnesses with different frontal and plan solidities. These are described in:
[1] Placidi, M., & Ganapathisubramani, B. (2015). Effects of frontal and plan solidities on aerodynamic parameters and the roughness sublayer in turbulent boundary layers. Journal of Fluid Mechanics, 782, 541–566. http://doi.org/10.1017/jfm.2015.552
[2] Placidi, M., & Ganapathisubramani, B. (2018). Turbulent Flow Over Large Roughness Elements: Effect of Frontal and Plan Solidity on Turbulence Statistics and Structure. Boundary-Layer Meteorology, 167, 99–121. http://doi.org/10.1007/s10546-017-0317-3
[3] 3] Placidi M. & Ganapathisubramani, B (2019). Velocity statistics for rough-wall turbulent boundary layer flow over LEGO roughness elements in different layouts. DOI: 10.5258/SOTON/D0829.
PLEASE CITE THESE PAPERS AND THIS DATASET DOI WHEN USING THE DATA.
Contact Dr Marco Placidi (m.placidi@surrey.ac.uk) or Prof Bharathram Ganapathisubramani (G.Bharath@soton.ac.uk) for any queries on the dataset.
$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$
Format of the dataset:
d = Virtual origin [mm]
delta = Boundary layer thickness (delta99 [mm])
deltas = Displacement thickness [mm]
dyn_visc_air = Air dynamic viscosity [Kg/(m s)]
h = Height of the roughness [mm]
K = Acceleration parameter as in [1]
rho_air = Air density [kq/m^3]
run = Case ID as in [1] and [2]
theta = Momentum thickness [mm]
U = Mean streamwise velocity [m/s]
U_edge = Mean streamwise velocity at the edge of the boundary layer [m/s]
utau = Skin friction velocity [m/s] based on drag measurements
uu = Streamwise velocity fluctuations
uv = Reynolds shear stresses
V = Mean wall-normal velocity [m/s]
vv = Wall-normal velocity fluctuations
X = Streamwise coordinate [mm]
Y = Wall-normal coordinate [mm]
y0 = Roughness length [mm]
Additional notes on the dataset:
- The 2D PIV dataset has been averaged across the Field of View in the streamwise direction to obtain 1D profiles.
- utau is measured directly by means of a floating-element drag balance as described in [1].
- y0,d, are obtained via best fitting the velocity profiles as in [1].
- The entire dataset has been filtered to match the local resolution for all cases, as discussed in [1].
- The acceleration parameter is defined in [1], and it is calculated from 2D PIV data across the size of the drag balance sensing element (i.e. 200 mm x200 mm). As such, it is affected by a significant experimental uncertainty. Additional verification of ZPG conditions were obtained via Pitot tube measurements between the inlet and outlet of the tunnel test section. The pressure gradient was considered negligible.
Archive
Lego_Dataset.zip
- Dataset
More information
Published date: 2 March 2019
Keywords:
Rough-wall boundary layer, LEGO roughness
Identifiers
Local EPrints ID: 428610
URI: http://eprints.soton.ac.uk/id/eprint/428610
PURE UUID: abb40886-70d0-4981-8bd8-a2e9aa48fc47
Catalogue record
Date deposited: 04 Mar 2019 17:31
Last modified: 13 Nov 2023 02:42
Export record
Altmetrics
Contributors
Creator:
M. Placidi
Download statistics
Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.
View more statistics