Explanation of the workbook More information:
http://www.dmu.dk/International/Air/Models/Background/MUST
Contents of this workbook
This Excel file contains sheets with short descriptions of model runs ('Group_and_Model') as well as Contact:
sheets with more detailed information ('Info_...'), derived from questionnaries on Geometry, Boundary Helge R. Olesen (hro@dmu.dk)
conditions, Physical parameters and Numerical Parameters.
The sheets are (besides this explanation):
Short descriptions:
Flow0_Group_and_model
Flow45_Group_and_model
Dispersion_CFD_Group_and_model
Log of changes
Dispersion_non_Group_and_model (concerns non-CFD models)
Details: Version Date Comment
Info_Flow0 ver1_001 11/28/2008 First public version of the workbook with model descriptions
Info_Flow45 ver1_002 12/5/2008 Name of Adrea run corrected.
Info_Disp
Info_Disp_nonCFD
Versions of the workbook
The first public version of the present workbook was released in November 2008 under the name
Description_ver1_001.xls.
Leading to the public version there was a series of versions, released internally in the COST 732 group.
0 degree flow case. Short description c31ca3c1-0699-4a66-bc89-761c976ee739.xls ! Flow0_Group_and_model 11/17/2011
OK to put
Boundary Physical Numerical
Run_ID Short Name Contact person INSTITUTION Model name, version Comments Geometry Run status on public Run date
conditions parameters parameters
web site?
K(eep) or P(ublic) or
V(ariation) - K I(nternal)
for most official
version(s) of
First name Last Name Email Department , University e.g FLUENT, CFD runs
Fl00_001 MISKAM_Ketzel Matthias Ketzel mke@dmu.dk NERI Denmark MISKAM vers. 5.01 Fine grid 4.4 Mio cells, 0.5m resolution within K P 14 Jan 2007
the building array, top boundary at 100m,
roughness 2cm everywhere on ground. A bug
in the procedure for wall boundary cond. can
lead to incorrect results close to walls. This
bug occurs in MISKAM v 5.0x
Show Show Show Show
Fl00_002 MISKAMcoarse_Ketzel Matthias Ketzel mke@dmu.dk NERI Denmark MISKAM vers. 5.01 Coarse grid, 2.2 Mio cells, 1m resolution V P 05 Dec 2006
within the buildings array, top boundary at
100m, roughness 2cm everywhere on ground
Show Show Show Show
Fl00_003 MISKAMcoarse20layer_Ketzel Matthias Ketzel mke@dmu.dk NERI Denmark MISKAM vers. 5.01 Coarse grid 1.5 Mio cells, 1m resolution within V P 04 Dec 2006
the building array, top boundary at 20m,
roughness 2cm everywhere on ground Show Show Show Show
Fl00_004 MISKAM1mres_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid MISKAM vers. 5.01 1 m res. Grid V P 01 Mar 2007
Mechanics, BME Hungary Show Show Show Show
Fl00_005 MISKAM08mres_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid MISKAM vers. 5.01 0.8 m res. Grid V P 01 Mar 2007
Mechanics, BME Hungary Show Show Show Show
Fl00_006 MISKAM05mres_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid MISKAM vers. 5.01 0.5 m res. Grid K P 01 Mar 2007
Mechanics, BME Hungary Show Show Show Show
Fl00_007 MISKAM_ZAMG Erwin Polreich erwin.polreich@zamg.ac.at ZAMG Austria MISKAM vers. 5.02 1m horizontal resolution. 10cm roughness. Show Show Show Show March 08(?)
Fl00_008 FLUENTske_DiSabatino Silvana Di Sabatino Riccardo Buccolieri silvana.disabatino@unile.it Dipartimento di Scienza dei FLUENT vers. 6.2.16 Turbulence model: standard k-epsilon; Lateral K P 13 Feb 2007
Materiali, University of and top boundary conditions: symmetry.
Salento, Lecce (Italy) Structured hexa mesh (~1.300.000 cells)
Show Show Show Show
Fl00_009 FLUENTrsm_DiSabatino Silvana Di Sabatino Riccardo Buccolieri silvana.disabatino@unile.it Dipartimento di Scienza dei FLUENT vers. 6.2.16 Turbulence model: RSMl; Lateral and top K P 13 Feb 2007
Materiali, University of boundary conditions: symmetry. Structured
Salento, Lecce (Italy) hexa mesh (~1.300.000 cells) Show Show Show Show
Fl00_010 FLUENTskeBCsym_Santiago Jose Luis Santiago jl.santiago@ciemat.es CIEMAT Spain FLUENT vers. 6.2.16 Turbulence model: standard k-epsilon; Lateral K P 13 Feb 2007
and top boundary conditions: symmetry
Show Show Show Show
Fl00_011 FLUENTskeBCwall_Santiago Jose Luis Santiago jl.santiago@ciemat.es CIEMAT Spain FLUENT vers. 6.2.16 Turbulence model: standard k-epsilon; Lateral V P 13 Feb 2007
and top boundary conditions: wall Show Show Show Show
Fl00_012 FLUENTrkeBCsym_Santiago Jose Luis Santiago jl.santiago@ciemat.es CIEMAT Spain FLUENT vers. 6.2.16 Turbulence model: Realizable k-epsilon; V P 13 Feb 2007
Lateral and top boundary conditions:
symmetry Show Show Show Show
Fl00_013 ADREA_Bartzis John Bartzis bartzis@uowm.gr Department of Engineering ADREA version 2, CFD Cartesian coordinate system with hexahedral K P 19 Nov 2007
and Management of Energy cells
Resources University of West
Macedonia Greece Show Show Show Show
Fl00_014 STAR_CD_Bartzis John Bartzis bartzis@uowm.gr Department of Engineering STAR-CD vers. 3.2, CFD Cartesian coordinate system with hexahedral K P 13 Feb 2007
and Management of Energy cells
Resources University of West
Macedonia Greece Show Show Show Show
Fl00_015 STAR_CD_doublegrid_Bartzis John Bartzis bartzis@uowm.gr Department of Engineering STAR-CD vers. 3.2, CFD Cartesian coordinate system with hexahedral K P 13 Feb 2007
and Management of Energy cells double grid in direction y
Resources University of West
Macedonia Greece Show Show Show Show
Fl00_016 Fluent_mskesp_Franke Jöerg Franke franke@ift.mb.uni-siegen.de IFT, University Siegen FLUENT V 6.2.16 medium grid, inflow bcs from periodic K P 05 Oct 2007
conditions, fixed values at top Show Show Show Show
Fl00_017 Fluent_mskespudf_Franke Jöerg Franke franke@ift.mb.uni-siegen.de IFT, University Siegen FLUENT V 6.2.16 medium grid, inflow bcs from Richards & K P 05 Oct 2007
Hoxey, fixed values at top Show Show Show Show
Fl00_018 Fluent_mskespudftsym_Franke Jöerg Franke franke@ift.mb.uni-siegen.de IFT, University Siegen FLUENT V 6.2.16 medium grid, inflow bcs from Richards & K P 07 Oct 2007
Hoxey, symmetry at top Show Show Show Show
Fl00_019 FluentFS1_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid Fluent 6.3.26 coarse grid (1.5 million cells) k-e V P 21 Nov 2007
Mechanics, BME Hungary realizable, non-equilibrium wall treatment,
single precision, Second Order Upwind, Full
Scale, Uref = 1 m/s Show Show Show Show
Fl00_020 FluentFS10_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid Fluent 6.3.26 coarse grid (1.5 million cells) k-e K P 21 Nov 2007
Mechanics, BME Hungary realizable, non-equilibrium wall treatment,
single precision, Second Order Upwind, Full
Scale, Uref = 10 m/s Show Show Show Show
Fl00_023 FINFLO_Hellsten Antti Hellsten antti.hellsten@tkk.fi Laboratory of Aerodynamics, FINFLO, CFD ?? K P 20 Feb 2007
Helsinki University of
Technology Show Show Show Show
Fl00_024 MITRAS2-10oC_Schluenzen Heinke Schlünzen heinke.schluenzen@zmaw.de Mi Uni Hamburg MITRAS Vers 2.2 fine grid, without Coriolisforce Show Show Show Show K P 02 Apr 2007
Fl00_026 CFX-unstr-ke_Fotios Fotios Barmpas fotisb@aix.meng.auth.gr AUTh, LHTEE, Greece CFX 5.7.1 Unstructuctured mesh, 1e-4 max. residuals K P 20 May 2007
conv. Criterion, Standard k-e Show Show Show Show
0 degree flow case. Short description c31ca3c1-0699-4a66-bc89-761c976ee739.xls ! Flow0_Group_and_model 11/17/2011
OK to put
Boundary Physical Numerical
Run_ID Short Name Contact person INSTITUTION Model name, version Comments Geometry Run status on public Run date
conditions parameters parameters
web site?
Fl00_027 CFX-str-ke_Fotios Fotios Barmpas fotisb@aix.meng.auth.gr AUTh, LHTEE, Greece CFX 5.7.1 Structured hexa mesh, 1e-4 max. residuals K P 20 May 2007
conv. Criterion, Standard k-e Show Show Show Show
Fl00_028 CFX-str-sst_Fotios Fotios Barmpas fotisb@aix.meng.auth.gr AUTh, LHTEE, Greece CFX 5.7.1 Structured hexa mesh, 1e-4 max. residuals K P 20 May 2007
conv. Criterion, k-ω Shear Stress Transport
(SST) Show Show Show Show
Fl00_029 CFX-str-ssg_Fotios Fotios Barmpas fotisb@aix.meng.auth.gr AUTh, LHTEE, Greece CFX 5.7.1 Structured hexa mesh, 1e-4 max. residuals K P 20 May 2007
conv. Criterion, SSG Reynold stress model Show Show Show Show
Fl00_030 CFX-unstr-ke_final_Fotios Fotios Barmpas fotisb@aix.meng.auth.gr AUTh, LHTEE, Greece CFX 5.7.1 Unstructuctured fine mesh, 1e-4 max. K P 29 May 2007
residuals conv. Criterion, Standard k-e Show Show Show Show
Fl00_031 STARCD_coarse_Brzozowski Krzysztof Brzozowski kbrzozowski@ath.bielsko.pl University of Bielsko-Biala, StarCD v. 3.26 Coarse grid, II order UpWind scheme, 1e-3 as V P June 2007
Poland conv. criterion, standard k-e, Wall cond. at
lateral boundaries Show Show Show Show
Fl00_032 STARCD_medium_Brzozowski Krzysztof Brzozowski kbrzozowski@ath.bielsko.pl University of Bielsko-Biala, StarCD v. 3.26 Medium grid, II order UpWind scheme, 1e-3 V P June 2007
Poland as conv. criterion, standard k-e, Wall cond. at
lateral boundaries Show Show Show Show
Fl00_033 STARCD_fine_Brzozowski Krzysztof Brzozowski kbrzozowski@ath.bielsko.pl University of Bielsko-Biala, StarCD v. 3.26 Fine grid, II order UpWind scheme, 1e-3 as K P June 2007
Poland conv. criterion, standard k-e, Wall cond. at
lateral boundaries Show Show Show Show
Fl00_034 M2UE_Nuterman_Baklanov Alexander Baklanov alb@dmi.dk DMI Denmark TSU vers. 1.0 coarse grid, II order MLU UpWind scheme, K P 29 Jun 2007
turbulence model: standard k-e, submitted
June 11 Show Show Show Show
Fl00_037 LASAT_ZAMG Erwin Polreich erwin.polreich@zamg.ac.at ZAMG Austria LASAT v2.14 diagnostic windfield Show Show Show Show K P - but not CFD
Fl00_038 Code_Saturne Bertrand Carissimo carissim@cerea.enpc.fr CEREA, Université Paris Est Code_Saturne 1.3.2 unstructured, finite volume 22-may-08
Open Source : retd.edf.fr/code_saturne
CGNS grid by J. Franke Show Show Show Show K P
-45 degree flow case. Short description c31ca3c1-0699-4a66-bc89-761c976ee739.xls ! Flow45_Group_and_model 11/17/2011
OK to put
Boundary Physical Numerical
Run_ID Short Name Contact person INSTITUTION Model name, version Comments Geometry Run status on public Run date
conditions parameters pararmeters
web site?
K(eep) or
V(ariation) -
K for most
official
version(s) of P(ublic) or
First name - Last Name Email Department , University e.g FLUENT, CFD runs I(nternal)
Fl45_001 MISKAM_Ketzel Matthias Ketzel mke@dmu.dk NERI Denmark MISKAM vers. 5.01 Fine grid 4.4 Mio cells, 0.5m resolution V P 22 Apr 2007
within the building array, top boundary at
100m, roughness 2cm everywhere on
ground. A bug in the procedure for wall
boundary cond. can lead to incorrect results
close to walls. This bug occurs in MISKAM
v 5.0x Show Show Show Show
Fl45_002 MISKAM_Ketzel_varRoughness Matthias Ketzel mke@dmu.dk NERI Denmark MISKAM vers. 5.01 fine grid 4.4 Mio cells, 0.5m resolution within K P 18 Jun 2007
the building array, top boundary at 100m,
roughness 0.2 cm within turntable,
otherwise 1 cm Show Show Show Show
Fl45_003 Miskam1mres_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid MISKAM vers. 5.01 1 m res. Grid V P Mar 07
Mechanics, BME Hungary Show Show Show Show
Fl45_004 Miskam08mres_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid MISKAM vers. 5.01 0.8 m res. Grid V P Mar 07
Mechanics, BME Hungary Show Show Show Show
Fl45_005 Miskam05mres_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid MISKAM vers. 5.01 0.5 m res. Grid K P Mar 07
Mechanics, BME Hungary Show Show Show Show
Fl45_006 MISKAM_ZAMG Erwin Polreich erwin.polreich@zamg.ac.at ZAMG Austria MISKAM vers. 5.02 1 m horizontal resolution. Roughness 10cm. K P 18 Jun 2008
Show Show Show Show
Fl45_007 FLUENT_Santiago Jose Luis Santiago jl.santiago@ciemat.es CIEMAT Spain FLUENT vers. 6.2.16 Turbulence model: standard k-epsilon; K P
Lateral and top boundary conditions:
symmetry. Mesh- Joerg Franke Show Show Show Show
Fl45_008 FLUENTske_DiSabatino Silvana Di Sabatino silvana.disabatino@unile.it Dipartimento di Scienza dei FLUENT vers. 6.2.16 Turbulence model: standard k-epsilon; K P 30 Mar 2007
Materiali, University of Lateral and top boundary conditions:
Salento, Lecce (Italy) symmetry. Structured hexa mesh
(~1.300.000 cells) Show Show Show Show
Fl45_009 Fluent_mrotskespudf_Franke Joerg Franke joerg.franke@uni-siegen.de IFT, Uni-Siegen, Germany FLUENT vers. 6.2.16 inflow rotated, inflow profiles from RH, fixed K P 02 Nov 2007
values at top, medium grid Show Show Show Show
Fl45_010 Fluent_mskesp_Franke Joerg Franke joerg.franke@uni-siegen.de IFT, Uni-Siegen, Germany FLUENT vers. 6.2.16 buildings rotated, inflow from periodic K P 08 Oct 2007
simulation, fixed values at top, medium grid
Show Show Show Show
Fl45_011 Fluent_mskespudf_Franke Joerg Franke joerg.franke@uni-siegen.de IFT, Uni-Siegen, Germany FLUENT vers. 6.2.16 buildings rotated, inflow from RH, fixed K P 08 Oct 2007
values at top, medium grid Show Show Show Show
Fl45_012 Fluent_mskespudftsym_Franke Joerg Franke joerg.franke@uni-siegen.de IFT, Uni-Siegen, Germany FLUENT vers. 6.2.16 buildings rotated, inflow from RH, symmetry K P 08 Oct 2007
at top, medium grid Show Show Show Show
Fl45_013 Fluent_ke_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid Fluent 6.3.26 k-e modell K P Nov 07
Mechanics, BME Hungary Show Show Show Show
Fl45_014 Fluent_RSM_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid Fluent 6.3.26 RSM modell (v'w'=u'w') K P Nov 07
Mechanics, BME Hungary Show Show Show Show
Fl45_015 STAR_CD_Bartzis John Bartzis bartzis@uowm.gr Department of Engineering STAR-CD vers. 3.22, CFD The computational grid was sent by Joerg K P June 07
and Management of Energy Franke, University of Siegen. Total number
Resources University of West of cells: 1,862,200
Macedonia Greece Show Show Show Show
Fl45_016 CFX-unstr-ke_fine_Fotios Fotios Barmpas fotis@aix.meng.auth.gr AUTH LHTEE CFX vers 5.7.1 unstructured grid, 5.5 million cells, K P July 07
corrected inflow BCs Show Show Show Show
Fl45_017 FINFLO_Hellsten1 Antti Hellsten antti.hellsten@fmi.fi TKK Finland FINFLO, CFD fine grid 3,600,000 cells Show Show Show Show K P June 07
Fl45_018 FINFLO_Hellsten2 Antti Hellsten antti.hellsten@fmi.fi TKK Finland FINFLO, CFD medium grid 450,000 cells Show Show Show Show K P June 07
Fl45_019 FINFLO_Hellsten3 Antti Hellsten antti.hellsten@fmi.fi TKK Finland FINFLO, CFD coarse grid 56,000 cells Show Show Show Show K P June 07
Fl45_020 M2UE_Nuterman_Baklanov Alexander Baklanov alb@dmi.dk DMI Denmark M2UE vers. 1.0 coarse grid 1.5 Mio cells, II order MLU K P 29 Jun 2007
upwind scheme, turbulence model:
standard k-e Show Show Show Show
Fl45_021 VADIS_Costa_2m Ana Margarida Costa amcosta@ua.pt UAVR Portugal VADIS, CFD coarse grid 459 375 cells Show Show Show Show V P Feb 08
Fl45_022 VADIS_Costa_1m Ana Margarida Costa amcosta@ua.pt UAVR Portugal VADIS, CFD Fine grid 3 675 000 cells Show Show Show Show V P Feb 08
Fl45_023 VADIS_Costa_0_5m Ana Margarida Costa amcosta@ua.pt UAVR Portugal VADIS, CFD Fine grid 29 400 000 cells Show Show Show Show K P Feb 08
Fl45_024 STARCD_coarse_Brzozowski Krzysztof Brzozowski kbrzozowski@ath.bielsko.pl University of Bielsko-Biala, StarCD v. 3.26 Coarse grid (about 0.5 M cells), II order V P June 07
Poland UpWind scheme, 1e-3 as conv. criterion,
standard k-e, Wall cond. at lateral
boundaries Show Show Show Show
Fl45_025 STARCD_medium_Brzozowski Krzysztof Brzozowski kbrzozowski@ath.bielsko.pl University of Bielsko-Biala, StarCD v. 3.26 Medium grid (about 1 M cells), II order V P June 07
Poland UpWind scheme, 1e-3 as conv. criterion,
standard k-e, Wall cond. at lateral
boundaries Show Show Show Show
Fl45_026 STARCD_fine_Brzozowski Krzysztof Brzozowski kbrzozowski@ath.bielsko.pl University of Bielsko-Biala, StarCD v. 3.26 Fine grid (more than 1.5 M cells), II order K P June 07
Poland UpWind scheme, 1e-3 as conv. criterion,
standard k-e, Wall cond. at lateral
boundaries Show Show Show Show
Fl45_027 ADREA_Bartzis John Bartzis bartzis@uowm.gr Department of Engineering ADREA Version 2 Cartesian coordinate system with K P October 07
and Management of Energy hexahedral cells
Resources University of West
Macedonia Greece Show Show Show Show
Fl45_028 LASAT_ZAMG Erwin Polreich k.baumann-stanzer@zamg.ac.at ZAMG Austria LASAT v2.14 particle diffusion model caluclation based on K 16-may-2008
P - but not CFD
a diagnostic windfield with rotated
coordinate system Show Show Show Show
Fl45_029 Code_Saturne Bertrand Carissimo carissim@cerea.enpc.fr CEREA, Université Paris Est Code_Saturne 1.3.2 unstructured, finite volume 22-may-2008
Open Source : retd.edf.fr/code_saturne
CGNS grid by J. Franke Show Show Show Show K P
-45 degree dispersion case. Short description c31ca3c1-0699-4a66-bc89-761c976ee739.xls ! Dispersion_CFD_Group_and_model 11/17/2011
OK to put
Boundary Physical Numerical Source
Run_ID Short Name Contact person INSTITUTION Model name, version Comments Geometry Run status on public Run date
conditions parameters parameters treatment
web site?
First name - Last Name Email Department , University e.g FLUENT, CFD K(eep) or
V(ariation) -
K for most
official
version(s) P(ublic) or
of runs I(nternal)
Disp_001 MISKAM_Ketzel Matthias Ketzel mke@dmu.dk NERI Denmark MISKAM vers. 5.01 Fine grid 4.4 Mio cells, roughness 2 cm V P 30 May 2007
everywhere on ground Show Show Show Show Show
Disp_002 MISKAM_Ketzel_varRoughness Matthias Ketzel mke@dmu.dk NERI Denmark MISKAM vers. 5.01 Roughness 0.2 cm within turntable, K P 18 Jun 2007
otherwise 1 cm Show Show Show Show Show
Disp_003 MISKAM1mres_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid Mechanics, BME MISKAM vers. 5.01 1 m res. Grid V P Mar 07
Hungary Show Show Show Show Show
Disp_004 MISKAM08mres_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid Mechanics, BME MISKAM vers. 5.01 0.8 m res. Grid V P Mar 07
Hungary Show Show Show Show Show
Disp_005 MISKAM05mres_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid Mechanics, BME MISKAM vers. 5.01 0.5 m res. Grid K P Mar 07
Hungary Show Show Show Show Show
Disp_006 MISKAM_ZAMG Erwin Polreich erwin.polreich@zamg.ac.at ZAMG Austria MISKAM vers. 5.02 1m horizontal resolution. 10cm K P 18 Jun 2008
roughness. Show Show Show Show Show
Disp_007 Fluent_ke_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid Mechanics, BME Fluent6.3.26 1.5 mio, k-e, Uref=10 m/s K P Nov 07
Hungary Show Show Show Show Show
Disp_008 Fluent_RSM_Goricsan Istvan Goricsan goricsan@ara.bme.hu Department of Fluid Mechanics, BME Fluent6.3.26 RSM (v'w'=u'w') K P Nov 07
Hungary Show Show Show Show Show
Disp_009 FLUENTske_DiSabatino Silvana Di Sabatino Riccardo Buccolieri silvana.disabatino@unile.it Dipartimento di Scienza dei Materiali, FLUENT vers. 6.2.16 Turbulence model: standard k-epsilon; K P 03 Oct 2007
University of Salento, Lecce (Italy) Lateral and top boundary conditions:
symmetry. Structured hexa mesh
(~1.300.000 cells) Show Show Show Show Show
Disp_010 FLUENT_Santiago Jose Luis Santiago jl.santiago@ciemat.es CIEMAT Spain FLUENT vers. 6.2.16 Turbulence model: standard k-epsilon; K P
Lateral and top boundary conditions:
symmetry. Mesh- Joerg Franke Show Show Show Show Show
Disp_011 Fluent_mskespudf_Franke Joerg Franke joerg.franke@uni-siegen.de IFT, Uni-Siegen, Germany FLUENT vers. 6.2.16 buildings rotated, inflow from RH, fixed K P 08 Oct 2007
values at top, medium grid Show Show Show Show Show
Disp_012 CFX-unstr-ke_fine_Fotios Fotios Barmpas fotisb@aix.meng.auth.gr AUTh LHTEE CFX vers.5.7.1 unstructured grid, 5.5 million cells, area K P October 07
source, corrected inflow BCs Show Show Show Show Show
Disp_013 FINFLO_Hellsten1 Antti Hellsten antti.hellsten@fmi.fi TKK Finland FINFLO, CFD fine grid 3,600,000 cells Show Show Show Show Show K P June 07
Disp_014 FINFLO_Hellsten2 Antti Hellsten antti.hellsten@fmi.fi TKK Finland FINFLO, CFD medium grid 450,000 cells Show Show Show Show Show K P June 07
Disp_015 FINFLO_Hellsten3 Antti Hellsten antti.hellsten@fmi.fi TKK Finland FINFLO, CFD coarse grid 56,000 cells Show Show Show Show Show K P June 07
Disp_016 M2UE_Nuterman_Baklanov Alexander Baklanov alb@dmi.dk DMI Denmark M2UE vers. 1.0 coarse grid 1.5 Mio cells, II order MLU K P 29 Jun 2007
upwind scheme, turbulence model:
standard k-e. Show Show Show Show Show
Disp_017 VADIS_Costa_2m Ana Margarida Costa amcosta@ua.pt UAVR Portugal VADIS, CFD coarse grid 459 375 cells Show Show Show Show Show V P Feb 08
Disp_018 VADIS_Costa_1m Ana Margarida Costa amcosta@ua.pt UAVR Portugal VADIS, CFD fine grid 3 675 000 cells Show Show Show Show Show V P Feb 08
Disp_019 VADIS_Costa_0_5m Ana Margarida Costa amcosta@ua.pt UAVR Portugal VADIS, CFD finest grid 29 400 000 cells Show Show Show Show Show K P Feb 08
Disp_020 STARCD_fine_Brzozowski Krzysztof Brzozowski kbrzozowski@ath.bielsko.pl University of Bielsko-Biala, POLAND StarCD v. 3.26 Fine grid (more than 1.5 M cells), II K P Dec 07
order UpWind scheme, 1e-3 as conv.
criterion, standard k-e, Wall cond. at
lateral boundaries Show Show Show Show Show
Disp_025 ADREA_Bartzis John Bartzis bartzis@uowm.gr Department of Engineering and ADREA Version 2 Cartesian coordinate system with K P October 08
Management of Energy Resources hexahedral cells. Rerun October 2008,
University of West Macedonia Greece Run ID changed from Disp_021 to
Disp_025. Show Show Show Show Show
Disp_022 LASAT_ZAMG Kathrin Baumann-Stanzer k.baumann-stanzer@zamg.ac.at AMG Austria
Z LASAT v2.14 Lagrangian particle dispersion K 16-May-2008
P - but not CFD
calculation based on flow and
turbulence data from a mass-
conserving diagnostic flow model (not a
CFD model) with rotated coordinate
system. Show Show Show Show Show
Disp_023 Code_Saturne Bertrand Carissimo carissim@cerea.enpc.fr CEREA, Université Paris Est Code_Saturne 1.3.2 unstructured, finite volume K P 22-May-2008
Open Source : retd.edf.fr/code_saturne
CGNS grid by J. Franke
Show Show Show Show Show
Disp_024 LASAT_ZAMG_MISKAMwind Kathrin Baumann-Stanzer k.baumann-stanzer@zamg.ac.at AMG Austria
Z LASAT v2.14 Lagrangian particle dispersion K 16-May-2008
P - but not CFD
calculation based on MISKAM wind
fields (MISKAM_ZAMG) Show Show Show Show Show
-45 degree dispersion case. Non-CFD. Short description c31ca3c1-0699-4a66-bc89-761c976ee739.xls ! Dispersion_non_Group_and_model 11/17/2011
OK to put
Run
Run_ID Short Name Contact person INSTITUTION Model name, version Comments Sheet with more info on public Run date
status
web site?
Department , University e.g FLUENT, CFD K(eep) or
V(ariation)
- K for
most
official
version(s) P(ublic) or
First name - Last Name Email of runs I(nternal)
DiNo_001 ESCAPE_FMI Kari Riikonen kari.riikonen@fmi.fi FMI Finland ESCAPE Gaussian Show K P Feb-08
DiNo_002 ADMS_DiSabatino Silvana Di Sabatino Riccardo Buccolieri silvana.disabatino@unile.it Dipartimento di Scienza dei Materiali, ADMS-Urban vers. 2.2, quasi-Gaussian 1) The area occupied by the buildings was replaced with a single
University of Salento, Lecce (Italy) Atmospheric Dispersion Modelling System value of surface roughness z0=0.269m, calculated by morphometric
method (Macdonald et al, 1998)
2) The same z0 as in wind tunnel experiments was used in the area
upwind of the buildings. Show K P Feb-08
DiNo_003 ADMSurban_Marina Marina Neophytou neophytou@ucy.ac.cy University of Cyprus, Engineering School ADMS_Urban Monin Obukhov length: 30m and surface heat flux: 0W/m^2 Show K P feb-08(?)
DiNo_004 ADMS_ZAMG Kathrin Baumann-Stanzer k.baumann-stanzer@zamg.ac.atZAMG, Austria ADMS-Urban v 2.0 NON-CFD (Gaussian modified for convective conditions); simulation Show K P Feb-08
with equivalent buildings
DiNo_005 OML_NERI1 Helge Rørdam Olesen hro@dmu.dk NERI, Denmark OML, Research version Plume model. Zo and u* estimated from vertical wind profile at source Show V P Feb-08
(close to upwind edge of building array), considering only heights
above 5 m. This Zo is not representative for the plume, but included
to illustrate the effect of roughness. Zo=0.037m.
DiNo_006 OML_NERI2 Helge Rørdam Olesen hro@dmu.dk NERI, Denmark OML, Research version Plume model. Zo and u* estimated from vertical wind profile in the Show K P Feb-08
middle of building array), considering only heights above 5 m. This Zo
is representative for the plume. Zo=0.3m.
DiNo_007 CALPUFF_Krajcovicova Jana Krajcovicova jkrajc@gmail.com Air Quality Department, Slovak CALPUFF version 5.711 - Lagrangian puff Show K P Oct-07
Hydrometeorological Institute, Slovakia model using three-dimensional meteorological CALPUFF, simple mode using vertical wind and turbulence profile
fields produced by CALMET diagnostic model; (profile.dat) and surface met. (surface.dat). Profile.dat based on
MUST WT approach flow data and measured turbulence in the
building area;. Z0 = 0.1m has been computed using Lettau formula.
0 degree flow case. Model parameters c31ca3c1-0699-4a66-bc89-761c976ee739.xls ! Info_Flow0 11/17/2011
Run_ID Short Name Geometry Boundary conditions
Total size of Computational domain (in m) Individual geometrical characteristics of the BC within the computational domain in non-dimensional terms (characteristic length, the
average height of the containers Hc with Hc = 2.54 m)
Ground surfaces
Buildings walls
Length Full scale Distance of inlet Distance of outlet Distance of the left Distance of the right
Width (span Distance of top boundary
(stream Height (FS)/Wind tunnel upstream of the downstream of the (direction of the flow) (direction of the flow) Upwind Ground Surface Downwind Ground Surface The buildings area Ground Surface The right hand side lateral plane (the The left hand side lateral plane (the
wise) above the containers
wise) scale (WS) containers array containers array lateral boundary lateral boundary Inlet plane (the x- plane) Outlet plane (the x+ plane) y- plane) y+ plane) The top plane
Fl00_001 MISKAM_Ketzel Rough wall, Zo=2cm, Rough wall, Zo=2cm, Rough wall, Zo=0.2cm,
Rough wall, Zo=2cm, k =u*2/0.3,e =u*3/0.4z1,
314 300 130 FS 24 32 50.8 20 20 k =u*2/0.3,e =u*3/0.4z1, k =u*2/0.3,e =u*3/0.4z1, k =u*2/0.3,e =u*3/0.4y1, d/dx=0 d/dx=0 d/dy=0 d/dy=0 fixed values
u*=0.4V||/ln(z1+Zo/Zo)
u*=0.4V||/ln(z1+Zo/Zo) u*=0.4V||/ln(z1+Zo/Zo) u*=0.4V||/ln(y1+Zo/Zo)
Fl00_002 MISKAMcoarse_Ketzel Rough wall, Zo=2cm, Rough wall, Zo=2cm, Rough wall, Zo=0.2cm,
Rough wall, Zo=2cm, k =u*2/0.3,e =u*3/0.4z1,
314 300 130 FS 24 32 50.8 20 20 k =u*2/0.3,e =u*3/0.4z1, k =u*2/0.3,e =u*3/0.4z1, k =u*2/0.3,e =u*3/0.4y1, d/dx=0 d/dx=0 d/dy=0 d/dy=0 fixed values
u*=0.4V||/ln(z1+Zo/Zo)
u*=0.4V||/ln(z1+Zo/Zo) u*=0.4V||/ln(z1+Zo/Zo) u*=0.4V||/ln(y1+Zo/Zo)
Fl00_003 MISKAMcoarse20layer_Ketzel Rough wall, Zo=2cm, Rough wall, Zo=2cm, Rough wall, Zo=0.2cm,
Rough wall, Zo=2cm, k =u*2/0.3,e =u*3/0.4z1,
314 300 21 FS 24 32 7.2 20 20 k =u*2/0.3,e =u*3/0.4z1, k =u*2/0.3,e =u*3/0.4z1, k =u*2/0.3,e =u*3/0.4y1, d/dx=0 d/dx=0 d/dy=0 d/dy=0 fixed values
u*=0.4V||/ln(z1+Zo/Zo)
u*=0.4V||/ln(z1+Zo/Zo) u*=0.4V||/ln(z1+Zo/Zo) u*=0.4V||/ln(y1+Zo/Zo)
Fl00_004 MISKAM1mres_Goricsan
u, v, w, k, e values are taken from
314 300 21 FS 24 32 7.2 20 20 wall function, rough wall, Zo=0.1m wall function, rough wall, Zo=0.1m wall function, rough wall, Zo=0.1m wall function, rough wall, Zo=0.01m Equilibrium profile with Zo = 1 cm roughness, u = 1 m/s at Zref= 7.29m no flux, d/dx=0 no flux, d/dy=0 no flux, d/dy=0 the top of the inlet profiles, and
kept constant, dp/dz=0
Fl00_005 MISKAM08mres_Goricsan
u, v, w, k, e values are taken from
314 300 130 FS 24 32 50.8 20 20 wall function, rough wall, Zo=0.1m wall function, rough wall, Zo=0.1m wall function, rough wall, Zo=0.1m wall function, rough wall, Zo=0.01m Equilibrium profile with Zo = 1 cm roughness, u = 1 m/s at Zref= 7.29m no flux, d/dx=0 no flux, d/dy=0 no flux, d/dy=0 the top of the inlet profiles, and
kept constant, dp/dz=0
Fl00_006 MISKAM05mres_Goricsan
u, v, w, k, e values are taken from
wall function, rough wall,
314 300 130 FS 24 32 50.8 20 20 wall function, rough wall, Zo=0.02m wall function, rough wall, Zo=0.02m wall function, rough wall, Zo=0.02m Equilibrium profile with Zo = 1 cm roughness, u = 1 m/s at Zref= 7.29m no flux, d/dx=0 no flux, d/dy=0 no flux, d/dy=0 the top of the inlet profiles, and
Zo=0.002m
kept constant, dp/dz=0
Fl00_007 MISKAM_ZAMG velocity components and k-e values
Rough wall, dP/dn = 0, Zo = 0.1m Rough wall, dP/dn = 0, Zo = 0.1m Rough wall, dP/dn = 0, Zo = 0.1m Rough wall, dp/dn = 0, Zo = 0.1m Logarithmic wind profile from Zref, U(Zref), Zo and stability no flux, d/dx=0 are given from the inlet profiles,
dP/dn = 0
Fl00_008 FLUENTske_DiSabatino 3.24 2.93 0.28 WS 6 16 6 4 4 Rough wall, roughness height Ks = Zo x 20 Smooth wall Smooth wall Smooth wall Equilibrium profiles of velocity u, k and epsilon Outflow Symmetry Symmetry Symmetry
Fl00_009 FLUENTrsm_DiSabatino 3.24 2.93 0.28 WS 6 16 6 4 4 Rough wall, roughness height Ks = Zo x 20 Smooth wall Smooth wall Smooth wall Equilibrium profiles of velocity u, k and epsilon Outflow Symmetry Symmetry Symmetry
Fl00_010 FLUENTskeBCsym_Santiago Inflow profiles. Velocity u and TKE from wind tunnel measurements.
Standard wall functions, Zo=0.017m, Standard wall functions, Zo=0.017m, Standard wall functions, Zo=0.017m, Standard wall functions Outflow Symmetry Symmetry Symmetry
For epsilon: epsilon=[ Cm^(3/4)*kinlet^(3/2) ] / k*z
Fl00_011 FLUENTskeBCwall_Santiago Inflow profiles. Velocity u and TKE from wind tunnel measurements.
Standard wall functions, Zo=0.017m, Standard wall functions, Zo=0.017m, Standard wall functions, Zo=0.017m, Standard wall functions Outflow Standard wall functions Standard wall functions Standard wall functions
For epsilon: epsilon=[ Cm^(3/4)*kinlet^(3/2) ] / k*z
Fl00_012 FLUENTrkeBCsym_Santiago Inflow profiles. Velocity u and TKE from wind tunnel measurements.
Standard wall functions, Zo=0.017m, Standard wall functions, Zo=0.017m, Standard wall functions, Zo=0.017m, Standard wall functions Outflow Symmetry Symmetry Symmetry
For epsilon: epsilon=[ Cm^(3/4)*kinlet^(3/2) ] / k*z
Fl00_013 ADREA_Bartzis Rough wall, Standard wall functions, Rough wall, Standard wall functions, Smooth walls, standard wall Inflow profiles. Velocity u and TKE from wind tunnel measurements.
345.7952 345.1668 19.4301 FS 35.046 34.10236 6.65 26.28 31.555 Rough wall, Standard wall functions, Zo=0.017m Inlet-outlet flows Inlet-outlet flows Inlet-outlet flows Symmetry
Zo=0.017m Zo=0.017m functions, Zo = 0.0004m Zref=7.29 m, U(Zref) = 6.5565 m/s
Fl00_014 STAR_CD_Bartzis Rough wall, Standard wall functions, Rough wall, Standard wall functions, Smooth walls, standard wall Inflow profiles. Velocity u and TKE from wind tunnel measurements.
300 314 21.06 FS 23.6 27.6 7.3 26.4 22 Rough wall, Standard wall functions, Zo=0.0165m d/dx=0, Constant (gauge) pressure Symmetry Symmetry Symmetry
Zo=0.0165m Zo=0.0165m functions Zref=7.29 m, U(Zref) = 8.0 m/s
Fl00_015 STAR_CD_doublegrid_Bartzis Rough wall, Standard wall functions, Rough wall, Standard wall functions, Smooth walls, standard wall Inflow profiles. Velocity u and TKE from wind tunnel measurements.
300 314 21.06 FS 23.6 27.6 7.3 26.4 22 Rough wall, Standard wall functions, Zo=0.0165m d/dx=0, Constant (gauge) pressure Symmetry Symmetry Symmetry
Zo=0.0165m Zo=0.0165m functions Zref=7.29 m, U(Zref) = 8.0 m/s
Fl00_016 Fluent_mskesp_Franke Rough wall in the region x 17226.5625 m^2), wall function Smooth wall, wall function approach Smooth wall, wall function approach Smooth wall, wall function approach d/dx=0, Constant (gauge) pressure Smooth wall, wall function approach Smooth wall, wall function approach
shorter domain with periodic boundary conditions in x-direction. quantities from equilibrium profiles,
approach, Zo = 0.0165m
Zo=0.0165m, dP/dz = 0
Fl00_017 Fluent_mskespudf_Franke Rough wall in the region x 17226.5625 m^2), wall function Smooth wall, wall function approach Smooth wall, wall function approach Smooth wall, wall function approach Equilibrium profiles of U, V, W, k, epsilon d/dx=0, Constant (gauge) pressure Smooth wall, wall function approach Smooth wall, wall function approach
quantities from equilibrium profiles,
approach, Zo = 0.0165m
Zo=0.0165m, dP/dz = 0
Fl00_018 Fluent_mskespudftsym_Franke Rough wall in the region x 17226.5625 m^2), wall function Smooth wall, wall function approach Smooth wall, wall function approach Smooth wall, wall function approach Equilibrium profiles of U, V, W, k, epsilon d/dx=0, Constant (gauge) pressure Smooth wall, wall function approach Smooth wall, wall function approach Symmetry
approach, Zo = 0.0165m
Fl00_019 FluentFS1_Goricsan
Rough wall, Zo=0.017m, non-equilibrium wall Rough wall, Zo=0.017m, non- Rough wall, Zo=0.017m, non-equilibrium Smooth walls, standard non- inlet conditions taken from wind tunnel measurements Zref=7.29 m,
314 300 21.06 FS 23 33 7.3 20 20 outflow symmetry symmetry symmetry
function equilibrium wall function wall function equilibrium wall function U(Zref) = 1 m/s
Fl00_020 FluentFS10_Goricsan
Rough wall, Zo=0.017m, non-equilibrium wall Rough wall, Zo=0.017m, non- Rough wall, Zo=0.017m, non-equilibrium Smooth walls, standard non- inlet conditions taken from wind tunnel measurements Zref=7.29 m,
314 300 21.06 FS 23 33 7.3 20 20 outflow symmetry symmetry symmetry
function equilibrium wall function wall function equilibrium wall function U(Zref) = 10 m/s
Fl00_023 FINFLO_Hellsten Smooth walls, Standard wall Smooth walls, Standard wall Smooth walls, Standard wall
314 300 21.06 FS 24 33 7.34 21 22 Rough wall, Zo=0.017m, Standard wall functions Smooth walls, Standard wall functions Smooth walls, Standard wall functions Inlet conditions taken by wind tunnel measurements Pressure given, d^2/dx^2=0 for other variables Pressure given, d^2/dx^2=0 for other variables
functions functions functions
Fl00_024 MITRAS2-10oC_Schluenzen Constant flux, wall function (logarithmic), Zo = Constant flux, wall function Constant flux, wall function (logarithmic), Rough wall, Zo = 0.0004m, Radiation boundary for boundary normal advection upstream, d/dx=0
d/dx=0 (for V, W, TKE, P). U is d/dx=0 (for U, W, TKE, P). V is d/dx=0 (for U, W, TKE, P). V is
Rigid lid with absorbing layers,
calculated with boundary normal calculated with boundary normal calculated with boundary normal
0.017m, dP/dn=0 (logarithmic), Zo = 0.017m, dP/dn=0 Zo = 0.017m, dP/dn=0 dP/dn=0 (for TKE, V, W, P) W=0, d/dz=0 (for U, V)
advective term using upstream advective term using upstream advective term using upstream
Fl00_026 CFX-unstr-ke_Fotios Rough wall, Zo=0.017m, Standard wall Rough wall, Zo=0.017m, Standard wall Smooth walls, Standard wall
314 300 21.06 FS 57.42 84.027 7.08 51.096 50.771 Rough wall, Zo=0.017m, Standard wall functions inlet conditions taken by wind tunnel measurements atmospheric conditions symmetry conditions symmetry conditions symmetry conditions
functions functions functions
Fl00_027 CFX-str-ke_Fotios Rough wall, Zo=0.017m, Standard wall Rough wall, Zo=0.017m, Standard wall Smooth walls, Standard wall
739 420 21.06 FS 142.42 424.027 7.08 111.096 110.771 Rough wall, Zo=0.017m, Standard wall functions inlet conditions taken by wind tunnel measurements atmospheric conditions symmetry conditions symmetry conditions symmetry conditions
functions functions functions
Fl00_028 CFX-str-sst_Fotios
Rough wall, Zo=0.017m, Automatic Rough wall, Zo=0.017m, Automatic wall Smooth walls, Automatic wall
739 420 21.06 FS 142.42 424.027 7.08 111.096 110.771 Rough wall, Zo=0.017m, Automatic wall functions inlet conditions taken by wind tunnel measurements atmospheric conditions symmetry conditions symmetry conditions symmetry conditions
wall functions functions functions
Fl00_029 CFX-str-ssg_Fotios Rough wall, Zo=0.017m, Standard wall Rough wall, Zo=0.017m, Standard wall Smooth walls, Standard wall
739 420 21.06 FS 142.42 424.027 7.08 111.096 110.771 Rough wall, Zo=0.017m, Standard wall functions inlet conditions taken by wind tunnel measurements atmospheric conditions symmetry conditions symmetry conditions symmetry conditions
functions functions functions
Fl00_030 CFX-unstr-ke_final_Fotios Rough wall, Zo=0.017m, Standard wall Rough wall, Zo=0.017m, Standard wall Smooth walls, Standard wall
314 300 21.06 FS 57.42 84.027 7.08 51.096 50.771 Rough wall, Zo=0.017m, Standard wall functions inlet conditions taken by wind tunnel measurements atmospheric conditions symmetry conditions symmetry conditions symmetry conditions
functions functions functions
Fl00_031 STARCD_coarse_Brzozowski Smooth walls, standard wall Inflow profiles for velocity u from wind tunnel measurements and Smooth walls, standard wall Smooth walls, standard wall
Rough wall, Zo = 0.0165m, Standard wall functions Smooth walls, standard wall functions Smooth walls, standard wall functions d/dx=0 symmetry conditions
functions espilon. Constant value for TKE functions functions
Fl00_032 STARCD_medium_Brzozowski Smooth walls, standard wall Inflow profiles for velocity u from wind tunnel measurements and Smooth walls, standard wall Smooth walls, standard wall
Rough wall, Zo = 0.0165m, Standard wall functions Smooth walls, standard wall functions Smooth walls, standard wall functions d/dx=0 symmetry conditions
functions espilon. Constant value for TKE functions functions
Fl00_033 STARCD_fine_Brzozowski Smooth walls, standard wall Inflow profiles for velocity u from wind tunnel measurements and Smooth walls, standard wall Smooth walls, standard wall
Rough wall, Zo = 0.0165m, Standard wall functions Smooth walls, standard wall functions Smooth walls, standard wall functions d/dx=0 symmetry conditions
functions espilon. Constant value for TKE functions functions
Fl00_034 M2UE_Nuterman_Baklanov Simplified Chieng & Launder wall functions (SCL), Simplified Chieng & Launder wall Simplified Chieng & Launder wall functions Simplified Chieng & Launder wall Inflow profile for U, TKE = 1.44 m^2/s^2, epsilon = 0.2 m^2/s^3, Zref = Simplified Chieng & Launder wall Simplified Chieng & Launder wall Simplified Chieng & Launder wall
270 287 21 FS 50 59.5 18.5 50 50 d/dx=0
Zo = 0.017m functions (SCL), Zo = 0.017m (SCL), Zo = 0.017m functions (SCL), Zo = 0.017m 8.78m, U(Zref) = 5.5 m/s functions (SCL), Zo = 0.017m functions (SCL), Zo = 0.017m functions (SCL), Zo = 0.017m
Fl00_037 LASAT_ZAMG Normal components to wall of (U,
No slip U, V, W=0 No slip U, V, W=0 No slip U, V, W=0 Periodic U, V, W Periodic U, V, W Periodic U, V, W Periodic U, V, W Open U,V,W=0
V, W) = 0
Fl00_038 Code_Saturne Rough wall, Zo=0.017m, Standard wall Rough wall, Zo=0.017m, Standard wall Rough wall, Zo=0.017m, Standard
300 314 21.06 FS 24 32 7.2 20 20 Rough wall, Zo=0.017m, Standard wall functions inlet conditions taken by wind tunnel measurements Pressure given, Neumann for other variables
symmetry conditions symmetry conditions symmetry conditions
functions functions wall functions
0 degree flow case. Model parameters c31ca3c1-0699-4a66-bc89-761c976ee739.xls ! Info_Flow0 11/17/2011
Run_ID Short Name Physical parameter Numerical parameters
Grid type Resolution in gridpoints (if variable, provide min/max) Cells heights / height of containers (if variable, provide min/max) Expansion ratio / cell Total cells (FV) / Approximations Convergence
volume change grid points (FD)
Reynolds-number h_cont*U_in(z_ref)/nu Turbulence model
The velocity-scale- The length-scale- Model version name or developers' names (for instance: std. k-epsilon, floor
Value reference length Model class Wall treatment determining variable if not determining variable Launder-Sharma k-epsilon, Launder-Reece-Rodi RSM, give also a Containers Between containers Container walls
turbulent kinetic energy (epsilon, omega other) literature reference if the model is not widely known)
Length Width Height Streamwise Lateral Streamwise Lateral Roof
Fl00_001 MISKAM_Ketzel Analytical solution in cell closest to the
1000000 Linear 2-equation model TKE epsilon Standard k-eps Cartesian 24 6 5 24 20 0.2 0.2 0.2 0.2 17226.5625 m^2), wall Equilibrium profiles of U, V, W, k, epsilon Smooth wall, wall function approach Smooth wall, wall function approach turbulence quantities from equilibrium profiles,
approach approach approach (gauge) pressure
function approach, Zo = 0.0165m Zo=0.0165m, dP/dz = 0
Fl45_010 Fluent_mskesp_Franke Rough wall in the region x 17226.5625 m^2), wall simulation in emplty and shorter domain with Smooth wall, wall function approach Smooth wall, wall function approach turbulence quantities from equilibrium profiles,
approach approach approach (gauge) pressure
function approach, Zo = 0.0165m periodic boundary conditions in x-direction. Zo=0.0165m, dP/dz = 0
Fl45_011 Fluent_mskespudf_Franke Rough wall in the region x 17226.5625 m^2), wall Equilibrium profiles of U, V, W, k, epsilon Smooth wall, wall function approach Smooth wall, wall function approach turbulence quantities from equilibrium profiles,
approach approach approach (gauge) pressure
function approach, Zo = 0.0165m Zo=0.0165m, dP/dz = 0
Fl45_012 Fluent_mskespudftsym_Franke Rough wall in the region x 17226.5625 m^2), wall Equilibrium profiles of U, V, W, k, epsilon Smooth wall, wall function approach Smooth wall, wall function approach Symmetry
approach approach approach (gauge) pressure
function approach, Zo = 0.0165m
Fl45_013 Fluent_ke_Goricsan Rough wall, Zo=0.017m, non-equilibrium wall
Rough wall, Zo=0.017m, Rough wall, Zo=0.017m, Smooth walls, standard
inlet conditions taken from wind tunnel
340 300 21.06 FS 16.6 17.3 7.3 7.75 8.28 non-equilibrium wall non-equilibrium wall non-equilibrium wall outflow Symmetry Symmetry Symmetry
function measurements Zref=7.29 m, U(Zref) = 10 m/s
function function function
Fl45_014 Fluent_RSM_Goricsan Rough wall, Zo=0.017m, non-equilibrium wall
Rough wall, Zo=0.017m, Rough wall, Zo=0.017m, Smooth walls, standard
inlet conditions taken from wind tunnel
340 300 21.06 FS 16.6 17.3 7.3 7.75 8.28 non-equilibrium wall non-equilibrium wall non-equilibrium wall outflow Symmetry Symmetry Symmetry
function measurements Zref=7.29 m, U(Zref) = 10 m/s
function function function
Fl45_015 STAR_CD_Bartzis Rough wall, Standard wall functions, Rough wall, Standard wall Rough wall, Standard wall Smooth walls, standard
Inflow profiles. Velocity u and TKE from wind
d/dx=0, Constant
300 300 21.06 FS 16.61 17.3 7.3 7.75 8.28 tunnel measurements. Zref=7.29 m, U(Zref) = Symmetry Symmetry Symmetry
Zo=0.0165m functions, Zo=0.0165m functions, Zo=0.0165m wall functions (gauge) pressure
8.0 m/s
Fl45_016 CFX-unstr-ke_fine_Fotios Rough wall, Zo=0.017m, Rough wall, Zo=0.017m, Smooth walls, Standard Inlet conditions taken by wind tunnel Atmospheric
314 300 21.06 FS 16.187 43.944 7.08 No lateral boundaries. Two faces defined as inlet and two as outletRough wall, Zo=0.017m, Standard wall functions Symmetry conditions Symmetry conditions Symmetry conditions
Standard wall functions Standard wall functions wall functions measurements conditions
Fl45_017 FINFLO_Hellsten1
314 300 21.06 FS Min. 30, max. 34 Min. 31, max. 47 7.34 No lateral boundaries. The 0 deg. grid is simply rotated 45 deg. and two vertical boundaries Standard wall as inlets and two aswalls, Standard
Smooth outlets.
Rough wall, Zo=0.017m, are specified functions
Smooth walls, Standard Smooth walls, Standard Inlet conditions taken by wind tunnel No lateral walls, see explanations in cells J21, P21 and Q21 see explanations in cells J21, P21 and d^2/dx^2=0 for other variables
Pressure given, d^2/dx^2=0 for other variables No lateral walls, Pressure given, Q21
wall functions wall functions wall functions measurements
Fl45_018 FINFLO_Hellsten2
314 300 21.06 FS Min. 30, max. 34 Min. 31, max. 47 7.34 No lateral boundaries. The 0 deg. grid is simply rotated 45 deg. and two vertical boundaries Standard wall as inlets and two aswalls, Standard
Smooth outlets.
Rough wall, Zo=0.017m, are specified functions
Smooth walls, Standard Smooth walls, Standard Inlet conditions taken by wind tunnel No lateral walls, see explanations in cells J22, P22 and Q22 see explanations in cells J22, P22 and d^2/dx^2=0 for other variables
Pressure given, d^2/dx^2=0 for other variables No lateral walls, Pressure given, Q22
wall functions wall functions wall functions measurements
Fl45_019 FINFLO_Hellsten3
314 300 21.06 FS Min. 30, max. 34 Min. 31, max. 47 7.34 No lateral boundaries. The 0 deg. grid is simply rotated 45 deg. and two vertical boundaries Standard wall as inlets and two aswalls, Standard
Smooth outlets.
Rough wall, Zo=0.017m, are specified functions
Smooth walls, Standard Smooth walls, Standard Inlet conditions taken by wind tunnel No lateral walls, see explanations in cells J23, P23 and Q23 see explanations in cells J23, P23 and d^2/dx^2=0 for other variables
Pressure given, d^2/dx^2=0 for other variables No lateral walls, Pressure given, Q23
wall functions wall functions wall functions measurements
Fl45_020 M2UE_Nuterman_Baklanov Simplified Chieng & Launder wall functions
Simplified Chieng & Simplified Chieng & Simplified Chieng & Inflow profile for U, V. TKE = 1.44 m^2/s^2,
Simplified Chieng & Launder wall functions
Inflow profile for U, V. TKE = 1.44
Simplified Chieng & Launder wall functions
270 287 21 FS Min. 50, max. 60 Min. 50, max. 60 18.5 No lateral boundaries. The 0 deg. grid is simply rotated 45 deg. and two vertical boundaries are specified as inlets and two as wall functions
Launder outlets. Launder wall functions Launder wall functions epsilon = 0.2 m^2/s^3, Zref = 8.78m, U(Zref) = d/dx=0 m^2/s^2, epsilon = 0.2 m^2/s^3, Zref
(SCL), Zo = 0.017m (SCL), Zo = 0.017m (SCL), Zo = 0.017m
(SCL), Zo = 0.017m (SCL), Zo = 0.017m (SCL), Zo = 0.017m 5.5 m/s = 8.78m, U(Zref) = 5.5 m/s
Fl45_021 VADIS_Costa_2m Power law wind profile, k and epsilon user
Wind and temperature profiles, direct input
Free, except for mass balance kept
250 250 20 FS 44 38 17 26 42 Wall function Wall function Wall function Wall function d/dx=0 or developed over unobstructed field till Symmetry
defined profiles correct
convergence
Fl45_022 VADIS_Costa_1m Power law wind profile, k and epsilon user
Wind and temperature profiles, direct input
Free, except for mass balance kept
250 250 20 FS 44 38 17 26 42 Wall function Wall function Wall function Wall function d/dx=0 or developed over unobstructed field till Symmetry
defined profiles correct
convergence
Fl45_023 VADIS_Costa_0_5m Power law wind profile, k and epsilon user
Wind and temperature profiles, direct input
Free, except for mass balance kept
250 250 20 FS 44 38 17 26 42 Wall function Wall function Wall function Wall function d/dx=0 or developed over unobstructed field till Symmetry
defined profiles correct
convergence
Fl45_024 STARCD_coarse_Brzozowski Rough wall, Zo = 0.0165m, Standard wall Smooth walls, standard Smooth walls, standard Smooth walls, standard
Inflow profiles for velocity u from wind tunnel
measurements and espilon. Constant value for d/dx=0 Smooth walls, standard wall functions Smooth walls, standard wall functions symmetry conditions
functions wall functions wall functions wall functions
TKE
Fl45_025 STARCD_medium_Brzozowski Rough wall, Zo = 0.0165m, Standard wall Smooth walls, standard Smooth walls, standard Smooth walls, standard
Inflow profiles for velocity u from wind tunnel
measurements and espilon. Constant value for d/dx=0 Smooth walls, standard wall functions Smooth walls, standard wall functions symmetry conditions
functions wall functions wall functions wall functions
TKE
Fl45_026 STARCD_fine_Brzozowski Rough wall, Zo = 0.0165m, Standard wall Smooth walls, standard Smooth walls, standard Smooth walls, standard
Inflow profiles for velocity u from wind tunnel
measurements and espilon. Constant value for d/dx=0 Smooth walls, standard wall functions Smooth walls, standard wall functions symmetry conditions
functions wall functions wall functions wall functions
TKE
Fl45_027 ADREA_Bartzis
Smooth walls, standard Inflow profiles. Velocity u and TKE from wind Inflow profiles. Velocity u and TKE
Rough wall, Standard wall Rough wall, Standard wall
345.7952 345.1668 19.4301 FS 35.046 34.10236 6.65 26.28 31.555 Rough wall, Standard wall functions, Zo=0.017m wall functions, Zo = tunnel measurements. Zref=7.29 m, U(Zref) = Inlet-outlet flows Inlet-outlet flows from wind tunnel measurements. Symmetry
functions, Zo=0.017m functions, Zo=0.017m
0.0004m 6.5565 m/s Zref=7.29 m, U(Zref) = 6.5565 m/s
Fl45_028 LASAT_ZAMG Normal components to
No slip U, V, W=0 No slip U, V, W=0 No slip U, V, W=0 Periodic U, V, W Periodic U, V, W Periodic U, V, W Periodic U, V, W Open U,V,W=0
wall of (U, V, W) = 0
Fl45_029 Code_Saturne Rough wall, Zo=0.017m, Rough wall, Zo=0.017m, Rough wall, Zo=0.017m, inlet conditions taken by wind tunnel
340 300 21.06 FS 16.6 17.3 7.3 7.75 8.28 Rough wall, Zo=0.017m, Standard wall functions Pressure given, Neumann for other variables
symmetry conditions symmetry conditions symmetry conditions
Standard wall functions Standard wall functions Standard wall functions measurements
-45 degree flow case. Model parameters c31ca3c1-0699-4a66-bc89-761c976ee739.xls ! Info_Flow45 11/17/2011
Run_ID Short Name Physical parameter Numerical parameters
Grid type Resolution in gridpoints (if variable, provide min/max) Cells heights / height of containers (if variable, provide min/max) Expansion ratio / Total cells (FV) / Approximations Convergence
cell volume change grid points (FD)
Reynolds-number h_cont*U_in(z_ref)/nu Turbulence model
The velocity-scale- The length-scale- Model version name or developers' names (for instance: std. k- floor
Value reference length Model class Wall treatment determining variable if not determining variable epsilon, Launder-Sharma k-epsilon, Launder-Reece-Rodi RSM, Containers Between containers Container walls
turbulent kinetic energy (epsilon, omega other) give also a literature reference if the model is not widely known)
Length Width Height Streamwise Lateral Streamwise Lateral Roof
Fl45_001 MISKAM_Ketzel Linear 2-equation Analytical solution in cell
1000000 epsilon Standard k-eps Cartesian 24 6 5 24 20 0.2 0.2 0.2 0.2 <= 1.2 4400550
model closest to the wall
Fl45_002 MISKAM_Ketzel_varRoughness Linear 2-equation Analytical solution in cell
1000000 epsilon Standard k-eps Cartesian 24 6 5 24 20 0.2 0.2 0.2 0.2 <= 1.2 4400550
model closest to the wall
Fl45_003 Miskam1mres_Goricsan Modified k-e (Kato, M. and Launder, B.E. (1993) ‘The modelling of
Cartesian,
turbulent flow around stationary and vibrating square cylinders’,
Wall
Linear 2-equation model functions epsilon non- 12 3 5 9 to 13 5 to 11 0.4 0.4 0.2 0.2 <= 1.2 1300320 1st order upwind 1.00E-03
López, S.D. (2002) Numerische Modellierung turbulenter
equidistant
Umströmungen von Gebäuden. PhD thesis, Univ. Bremen: Germany
174000
Fl45_004 Miskam08mres_Goricsan Modified k-e (Kato, M. and Launder, B.E. (1993) ‘The modelling of
Cartesian,
turbulent flow around stationary and vibrating square cylinders’,
Wall
Linear 2-equation model functions epsilon non- 15 3 5 15 to 19 7 to 14 0.32 0.32 0.2 0.2 <= 1.2 3052560 1st order upwind 1.00E-03
López, S.D. (2002) Numerische Modellierung turbulenter
equidistant
Umströmungen von Gebäuden. PhD thesis, Univ. Bremen: Germany
174000
Fl45_005 Miskam05mres_Goricsan Modified k-e (Kato, M. and Launder, B.E. (1993) ‘The modelling of
Cartesian,
turbulent flow around stationary and vibrating square cylinders’,
Wall
Linear 2-equation model functions epsilon non- 24 5 5 11 to 28 10 to 18 0.2 0.2 0.2 0.2 <= 1.2 4788000 1st order upwind 1.00E-03
López, S.D. (2002) Numerische Modellierung turbulenter
equidistant
Umströmungen von Gebäuden. PhD thesis, Univ. Bremen: Germany
174000
Fl45_006 MISKAM_ZAMG 1392000 Linear 2-equation TKE 3600000 1st order upwind 0.001
Wall functions? epsilon Standard k-eps?
model
Fl45_007 FLUENT_Santiago Linear 2-equation
520000 Standard wall functions epsilon Standard k-eps block struct. 11//18 5 11 7//14 14//15 0.229//0.283 0.228//0.387 0.079 0.138 1675712 2nd order upwind 0.000001
model
Fl45_008 FLUENTske_DiSabatino Linear 2-equation
100000 Standard wall functions epsilon Standard k-eps hexahedral 12 2 13 13 8 0.08 0.08 0.16 0.08 <=1.3 ~1.100.000 2nd order upwind 0.000001
model
Fl45_009 Fluent_mrotskespudf_Franke
170000 Linear 2-equation
epsilon Standard k-eps block struct. 11//18 5 11 7//14 14//15 0.229//0.283 0.228//0.387 0.079 0.138 <= 1.3 1552792 2nd order upwind 0.000001
model
Rough wall-functions (Cs = 1.0)
Fl45_010 Fluent_mskesp_Franke
170000 Linear 2-equation
epsilon Standard k-eps block struct. 11//18 5 11 7//14 14//15 0.229//0.283 0.228//0.387 0.079 0.138 <= 1.3 1675712 2nd order upwind 0.000001
model
Rough wall-functions (Cs = 1.0)
Fl45_011 Fluent_mskespudf_Franke
170000 Linear 2-equation
epsilon Standard k-eps block struct. 11//18 5 11 7//14 14//15 0.229//0.283 0.228//0.387 0.079 0.138 <= 1.3 1675712 2nd order upwind 0.000001
model
Rough wall-functions (Cs = 1.0)
Fl45_012 Fluent_mskespudftsym_Franke
170000 Linear 2-equation
epsilon Standard k-eps block struct. 11//18 5 11 7//14 14//15 0.229//0.283 0.228//0.387 0.079 0.138 <= 1.3 1675712 2nd order upwind 0.000001
model
Rough wall-functions (Cs = 1.0)
Fl45_013 Fluent_ke_Goricsan Advanced linear 2- Special non-equailibrium wall Until residuals
functions, S.-E. Kim and Realizable k-eps by Shih et al. Computers Fluids, 24(3):227-238,
1738851 equation model epsilon hexahedral 11//18 5 11 7//14 14//15 0.229//0.283 0.228//0.387 0.079 0.138 <= 1.3 1675712 2nd order upwind stop changing
D. Choudhury. In ASME FED 1995.
(variable Cmu) Linear pressure strain model in Fluent, (M. M. Gibson and B. E. (~1e-5)
Vol. 217, Separated and
Fl45_014 Fluent_RSM_Goricsan Non-equilibrium wall-function, Launder. Ground Effects on Pressure Fluctuations in the Atmospheric Until residuals
1738851 RSM Wall BC from k, wall reflection epsilon Boundary Layer. J. Fluid Mech., 86:491-511, 1978., S. Fu, B. E. hexahedral 11//18 5 11 7//14 14//15 0.229//0.283 0.228//0.387 0.079 0.138 <= 1.3 1675712 2nd order upwind stop changing
effects Launder, and M. A. Leschziner. Modeling Strongly Swirling (~1e-5)
Fl45_015 STAR_CD_Bartzis Linear 2-equation
1353000 7.29 Standard wall functions epsilon Standard k-eps block struct. 11//18 5 11 7//14 14//15 0.229//0.283 0.228//0.387 0.079 0.138 <= 1.3 1675712 1st order upwind 0.001
model
Fl45_016 CFX-unstr-ke_fine_Fotios Unstructure 1e-4, MAX
813000 Standard wall functions epsilon Standard k-eps ~20 ~12 ~12 ~20 ~20 0.15 0.15 0.15 0.15 1.2 5500000 2nd order upwind
grid residuals
Fl45_017 FINFLO_Hellsten1 Third-order
26240 Linear 2-equation Standard k-eps transformed into the k-omega form, i.e. Menter's BSL Block Until residuals
Standard wall functions omega 24 8 12 16 12 0.125 0.125 0.0833 0.0833 upwind biased
model model with the blending function F1=0 everywhere. structured stop decreasing
scheme for fluxes
1.16 3599616
Fl45_018 FINFLO_Hellsten2 Third-order
26240 Linear 2-equation Standard k-eps transformed into the k-omega form, i.e. Menter's BSL Block Until residuals
Standard wall functions omega 12 4 6 8 6 0.25 0.25 0.167 0.167 449952 upwind biased
model model with the blending function F1=0 everywhere. structured stop decreasing
scheme for fluxes
1.16
Fl45_019 FINFLO_Hellsten3 Third-order
26240 Linear 2-equation Standard k-eps transformed into the k-omega form, i.e. Menter's BSL Block Until residuals
Standard wall functions omega 6 2 3 4 3 0.5 0.5 0.333 0.333 1.34 56244 upwind biased
model model with the blending function F1=0 everywhere. structured stop decreasing
scheme for fluxes
Fl45_020 M2UE_Nuterman_Baklanov Linear 2-equation
776000 Wall functions TKE epsilon Standard k-eps Cartesian ~10 ~5 ~10 ~10 ~5 1.29 1.58 0.74 0.25 1466828 2nd order MLU 0.001
model
Fl45_021 VADIS_Costa_2m Linear 2-equation 0.01 reached,
1920000 Wall functions epsilon Standard k-eps Cartesian Cartesian 6 1 1 8 0.787 0.787 0.787 0.787 157000 2nd order upwind
model 0.001 prescribed
Fl45_022 VADIS_Costa_1m Linear 2-equation 0.01 reached,
1920000 Wall functions epsilon Standard k-eps Cartesian Cartesian 12 2 2 16 0.394 0.394 0.394 0.394 3675000 2nd order upwind
model 0.001 prescribed
Fl45_023 VADIS_Costa_0_5m Linear 2-equation 0.01 reached,
1920000 Wall functions epsilon Standard k-eps Cartesian Cartesian 24 4 4 32 0.197 0.197 0.197 0.197 29400000 2nd order upwind
model 0.001 prescribed
Fl45_024 STARCD_coarse_Brzozowski Linear 2-equation Block
934000 Wall functions epsilon Standard k-eps 3//6 3 9//12 6 2//6 0.516/0.783 0.626/0.764 0.078 0.078 <= 1.2 457766 2nd order upwind 0.001
model structured
Fl45_025 STARCD_medium_Brzozowski Linear 2-equation Block
934000 Wall functions epsilon Standard k-eps 4//9 4 9//12 9 4//12 0.323/0.386 0.268/0.413 0.078 0.078 <= 1.2 959766 2nd order upwind 0.001
model structured
Fl45_026 STARCD_fine_Brzozowski Linear 2-equation Block
934000 Wall functions epsilon Standard k-eps 5//14 6 9//12 14 6//18 0.165/0.216 0.177/0.244 0.078 0.078 <= 1.2 1658152 2nd order upwind 0.001
model structured
Fl45_027 ADREA_Bartzis 0.0001 (0.001 for
Linear 2-equation Bartzis k-zeta model, Boundary-layer Meteorology (2005) 116: 445- turbulence and
1362000 7.29 Special surface-layer functions zeta (zeta=eps/(k^1.5)) Cartesian 4//5 2 8 10 5 0.48 1.2//0.96 0.277 0.125 <= 1.1 551936 1st order upwind
model 459 0.00000001 for
concentration)
Fl45_028 LASAT_ZAMG
Fl45_029 Code_Saturne
2-equation model epsilon Standard k-eps 11//18 5 11 7//14 14//15 0.229//0.283 0.228//0.387 0.079 0.138 <= 1.3 1675712 1st order upwind
1740000 Rough wall-functions unstructured 600 it
-45 degree dispersion case.CFD model parameters c31ca3c1-0699-4a66-bc89-761c976ee739.xls ! Info_Disp 11/17/2011
Run_ID Short Name Geometry Boundary conditions Physical parameter
Total size of Computational domain (in m) Individual geometrical characteristics of the BC within the computational domain in non-dimensional terms (characteristic length,
the average height of the containers H c with Hc = 2.54 m) Ground surfaces Reynolds-number h_cont*U_in(z_ref)/nu
Buildings walls
Length Full scale Distance of inlet Distance of outlet Distance of top Distance of the left Distance of the right
Width (span The buildings area Ground
(stream Height (FS)/Wind tunnel upstream of the downstream of the boundary above the (direction of the flow) (direction of the flow) Upwind Ground Surface Downwind Ground Surface Outlet plane (the The right hand side lateral plane (the y- The left hand side lateral plane (the y+ Value reference length Model class
wise) Surface
wise) scale (WS) containers array containers array containers lateral boundary lateral boundary Inlet plane (the x- plane) x+ plane) plane) plane) The top plane
Disp_001 MISKAM_Ketzel Linear 2-
314 300 130 FS 24 32 50.8 20 20 d/dz=0 ? d/dz=0 ? d/dz=0 ? d/dy=0 ? 0 d/dx=const d/dy=const d/dy=const ? 1000000 equation
model
Disp_002 MISKAM_Ketzel_varRoughness Linear 2-
314 300 130 FS 24 32 50.8 20 20 d/dz=0 ? d/dz=0 ? d/dz=0 ? d/dy=0 ? 0 d/dx=const d/dy=const d/dy=const ? 1000000 equation
model
Disp_003 MISKAM1mres_Goricsan
No lateral boundaries. The
0 deg. grid is simply u, v, w, k, e values are taken
rotated 45 deg. and two wall function, rough wall, wall function, rough wall, wall function, rough wall, Equilibrium profile with Zo = 1 cm from the top of the inlet
314 300 21 FS 20-23 20-33 7.2 wall function, rough wall, Zo=0.1m no flux, d/dx=0 no flux, d/dy=0 no flux, d/dy=0 Linear 2-equation model
vertical boundaries are Zo=0.1m Zo=0.1m Zo=0.01m roughness, u = 1 m/s at Zref= 7.29m profiles, and kept constant,
specified as inlets and two dp/dz=0
as outlets.
174000
Disp_004 MISKAM08mres_Goricsan No lateral boundaries. The
0 deg. grid is simply u, v, w, k, e values are taken
rotated 45 deg. and two wall function, rough wall, wall function, rough wall, wall function, rough wall, Equilibrium profile with Zo = 1 cm from the top of the inlet
314 300 130 FS 20-23 20-33 7.2 wall function, rough wall, Zo=0.1m no flux, d/dx=0 no flux, d/dy=0 no flux, d/dy=0 Linear 2-equation model
vertical boundaries are Zo=0.1m Zo=0.1m Zo=0.01m roughness, u = 1 m/s at Zref= 7.29m profiles, and kept constant,
specified as inlets and two dp/dz=1
as outlets.
174000
Disp_005 MISKAM05mres_Goricsan No lateral boundaries. The
0 deg. grid is simply u, v, w, k, e values are taken
rotated 45 deg. and two wall function, rough wall, wall function, rough wall, wall function, rough wall, wall function, rough wall, Equilibrium profile with Zo = 1 cm from the top of the inlet
314 300 130 FS 20-23 20-33 7.2 no flux, d/dx=0 no flux, d/dy=0 no flux, d/dy=0 Linear 2-equation model
vertical boundaries are Zo=0.02m Zo=0.02m Zo=0.02m Zo=0.002m roughness, u = 1 m/s at Zref= 7.29m profiles, and kept constant,
specified as inlets and two dp/dz=2
as outlets.
174000
Disp_006 MISKAM_ZAMG Rough wall, dP/dn = 0, Zo Rough wall, dP/dn = 0, Zo = Rough wall, dP/dn = 0, Zo = Rough wall, dp/dn = 0, Zo = Logarithmic wind profile from Zref,
velocity components and k-e Linear 2-
no flux, d/dx=0 values are given from the inlet 1392000 equation
= 0.1m 0.1m 0.1m 0.1m U(Zref), Zo and stability
profiles, dP/dn = 0 model
Disp_007 Fluent_ke_Goricsan Advanced
linear 2-
inlet conditions taken from wind tunnel
Rough wall, Zo=0.017m, Rough wall, Zo=0.017m, non- Rough wall, Zo=0.017m, non- Smooth walls, standard non- equation
340 300 21.06 FS 16.6 17.3 7.3 7.75 8.28 measurements Zref=7.29 m, U(Zref) = outflow Symmetry Symmetry Symmetry 1738851
non-equilibrium wall function equilibrium wall function equilibrium wall function equilibrium wall function model
10 m/s
(variable
Cmu)
Disp_008 Fluent_RSM_Goricsan
inlet conditions taken from wind tunnel
Rough wall, Zo=0.017m, Rough wall, Zo=0.017m, non- Rough wall, Zo=0.017m, non- Smooth walls, standard non-
340 300 21.06 FS 16.6 17.3 7.3 7.75 8.28 measurements Zref=7.29 m, U(Zref) = outflow Symmetry Symmetry Symmetry 1738851 RSM
non-equilibrium wall function equilibrium wall function equilibrium wall function equilibrium wall function
10 m/s
Disp_009 FLUENTske_DiSabatino Rough wall, roughness Equilibrium profiles of velocity u, k and
Linear 2-
325 280 27.5 FS 6 16 8 4 4 Smooth wall Smooth wall Smooth wall Outflow Symmetry Symmetry Symmetry 100000 equation
height Ks = Zo x 20 epsilon
model
Disp_010 FLUENT_Santiago Rough wall. SpecifiedGradient Linear 2-
Rough wall. SpecifiedGradient Rough wall. SpecifiedGradient Smooth wall. SpecifiedGradient SpecifiedGradient normal to plane, SpecifiedGradient normal to plane, SpecifiedGradient normal to
SpecifiedGradient normal to C=0 normal to plane, 520000 equation
normal to plane, dC/dn=0 normal to plane, dC/dn=0 normal to plane, dC/dn=0 dC/dn=0 dC/dn=0 plane, dC/dn=0
plane, dC/dn=0 dC/dn=0 model
Disp_011 Fluent_mskespudf_Franke Rough wall, logarithmic wall Smooth wall, logarithmic wall Smooth wall, logarithmic wall
Linear 2-
dC/dn=0 C=0 dC/dx=0 dC/dy=0 dC/dy=0 dC/dz=0 170000 equation
function function function
model
Disp_012 CFX-unstr-ke_fine_Fotios No lateral boundaries. Two
Rough wall, Zo=0.017m, Rough wall, Zo=0.017m, Rough wall, Zo=0.017m, Standard Smooth walls, Standard wall Inlet conditions taken by wind tunnel Atmospheric
Linear 2-
314 300 21.06 FS 16.187 43.944 7.08 faces defined as inlet and Symmetry conditions Symmetry conditions Symmetry conditions 813000 equation
Standard wall functions Standard wall functions wall functions functions measurements conditions
two as outlet model
Disp_013 FINFLO_Hellsten1 No lateral boundaries. The
0 deg. grid is simply
Pressure given, Linear 2-
rotated 45 deg. and two Rough wall, Zo=0.017m, Smooth walls, Standard wall Smooth walls, Standard wall Smooth walls, Standard wall Inlet conditions taken by wind tunnel No lateral walls, see explanations in cells No lateral walls, see explanations in cells Pressure given, d^2/dx^2=0
314 300 21.06 FS Min. 30, max. 34 Min. 31, max. 47 7.34 d^2/dx^2=0 for 26240 equation
vertical boundaries are Standard wall functions functions functions functions measurements J21, P21 and Q21 J21, P21 and Q21 for other variables
other variables model
specified as inlets and two
as outlets.
Disp_014 FINFLO_Hellsten2 No lateral boundaries. The
0 deg. grid is simply
Pressure given, Linear 2-
rotated 45 deg. and two Rough wall, Zo=0.017m, Smooth walls, Standard wall Smooth walls, Standard wall Smooth walls, Standard wall Inlet conditions taken by wind tunnel No lateral walls, see explanations in cells No lateral walls, see explanations in cells Pressure given, d^2/dx^2=0
314 300 21.06 FS Min. 30, max. 34 Min. 31, max. 47 7.34 d^2/dx^2=0 for 26240 equation
vertical boundaries are Standard wall functions functions functions functions measurements J22, P22 and Q22 J22, P22 and Q22 for other variables
other variables model
specified as inlets and two
as outlets.
Disp_015 FINFLO_Hellsten3 No lateral boundaries. The
0 deg. grid is simply
Pressure given, Linear 2-
rotated 45 deg. and two Rough wall, Zo=0.017m, Smooth walls, Standard wall Smooth walls, Standard wall Smooth walls, Standard wall Inlet conditions taken by wind tunnel No lateral walls, see explanations in cells No lateral walls, see explanations in cells Pressure given, d^2/dx^2=0
314 300 21.06 FS Min. 30, max. 34 Min. 31, max. 47 7.34 d^2/dx^2=0 for 26240 equation
vertical boundaries are Standard wall functions functions functions functions measurements J23, P23 and Q23 J23, P23 and Q23 for other variables
other variables model
specified as inlets and two
as outlets.
Disp_016 M2UE_Nuterman_Baklanov No lateral boundaries. The
0 deg. grid is simply
Inflow profile for U, V. TKE = 1.44 Linear 2-
rotated 45 deg. and two
270 287 21 FS Min. 50, max. 60 Min. 50, max. 60 18.5 d/dz=0 d/dz=0 d/dz=0 d/dn=0 m^2/s^2, epsilon = 0.2 m^2/s^3, Zref = d/dx=0 No lateral walls, see explanations in cell J No lateral walls, see explanations in cell J d/dz=0 776000 equation
vertical boundaries are
8.78m, U(Zref) = 5.5 m/s model
specified as inlets and two
as outlets.
Disp_017 VADIS_Costa_2m Power law wind profile, k and epsilon
Wind and temperature profiles, direct
Free, except for mass balance kept
Linear 2-
250 250 20 FS 44 38 17 26 42 Wall function Wall function Wall function Wall function d/dx=0 input or developed over unobstructed Symmetry 1920000 equation
user defined profiles correct
field till convergence model
Disp_018 VADIS_Costa_1m Power law wind profile, k and epsilon
Wind and temperature profiles, direct
Free, except for mass balance kept
Linear 2-
250 250 20 FS 44 38 17 26 42 Wall function Wall function Wall function Wall function d/dx=0 input or developed over unobstructed Symmetry 1920000 equation
user defined profiles correct
field till convergence model
Disp_019 VADIS_Costa_0_5m Power law wind profile, k and epsilon
Wind and temperature profiles, direct
Free, except for mass balance kept
Linear 2-
250 250 20 FS 44 38 17 26 42 Wall function Wall function Wall function Wall function d/dx=0 input or developed over unobstructed Symmetry 1920000 equation
user defined profiles correct
field till convergence model
Disp_020 STARCD_fine_Brzozowski Linear 2-
dC/dz=0 dC/dz=0 dC/dz=0 dC/dn=0 C=0 dC/dx=0 dC/dy=0 dC/dy=0 dC/dz=0 934000 equation
model
Disp_025 ADREA_Bartzis
Linear 2-
345.7952 345.1668 19.4301 FS 35.046 34.10236 6.65 26.28 31.555 dC/dz=0 dC/dz=0 dC/dz=0 dC/dn=0 C=0, dC/dx=0 dC/dx=0 dC/dy=0 C=0, dC/dy=0 dC/dz=0 1362000 7.29 equation
model
Disp_022 LASAT_ZAMG Zo = 0.8m Zo = 0.8m Zo = 0.8m dC/dn=0 open open open open open
Disp_023 Code_Saturne Linear 2-
340 300 21.06 FS 16.6 17.3 7.3 7.75 8.28 dC/dz=0 dC/dz=0 dC/dz=0 dC/dn=0 C=0 dC/dx=0 dC/dy=0 dC/dy=0 dC/dz=0 equation
1740000 model
Disp_024 LASAT_ZAMG_MISKAMwind Zo = 0.8m Zo = 0.8m Zo = 0.8m dC/dn=0 open open open open open
-45 degree dispersion case.CFD model parameters c31ca3c1-0699-4a66-bc89-761c976ee739.xls ! Info_Disp 11/17/2011
Run_ID Short Name Physical parameter Numerical parameters Source
Grid type Resolution in gridpoints (if variable, provide min/max) Cells heights / height of containers (if variable, provide min/max) Expansion ratio / Total cells (FV) / Approximations Convergence Source grid dimension.
Turbulence model cell volume change grid points (FD) DX*DY*DZ (m) or other
specification
The velocity-scale- The length-scale- Model version name or developers' names (for instance: std. k- Schmidt floor
Wall treatment determining variable if not determining variable epsilon, Launder-Sharma k-epsilon, Launder-Reece-Rodi RSM, give number Containers Between containers Container walls
turbulent kinetic energy (epsilon, omega other) also a literature reference if the model is not widely known).
Length Width Height Streamwise Lateral Streamwise Lateral Roof
Disp_001 MISKAM_Ketzel Analytical solution in cell closest
epsilon Standard k-eps, Sc=0.74 Sc=0.74 Cartesian 3 to 6 12 to 24 5 12 to 24 7 to 14 0.2 0.2 0.2 0.2 <= 1.2 4400550 0.5*1.0*0.5 (in
to the wall
model coordinates)
Disp_002 MISKAM_Ketzel_varRoughness Analytical solution in cell closest
epsilon Standard k-eps, Sc=0.74 Sc=0.74 Cartesian 3 to 6 12 to 24 5 12 to 24 7 to 14 0.2 0.2 0.2 0.2 <= 1.2 4400550 0.5*1.0*0.5 (in
to the wall
model coordinates)
Disp_003 MISKAM1mres_Goricsan modified k-e (Kato, M. and Launder, B.E. (1993) ‘The modelling of Flow: 1st order upwind; Dispersion:
turbulent flow around stationary and vibrating square cylinders’, Ninth MPDATA scheme (Smolarkiewicz, P. K.
Symposium on Turbulent Shear Flows, Kyoto, Japan, August 1993; and W. W. Grabowski, 1989: The
Cartesian, non-
Wall functions epsilon López, S.D. (2002) Numerische Modellierung turbulenter Sc=0.74 3 12 5 9 to 13 5 to 11 0.4 0.4 0.2 0.2 <= 1.2 1300320 multidimensional positive definite 1.00E-03 1 * 1 * 0.5
equidistant
Umströmungen von Gebäuden. PhD thesis, University of Bremen: advection transport algorithm:
Germany) ; dispersion: Reynolds-averaged advection-diffusion Nonoscillatory option. J. Compu.
equation Physics, 86, 355{375.)
Disp_004 MISKAM08mres_Goricsan modified k-e (Kato, M. and Launder, B.E. (1993) ‘The modelling of Flow: 1st order upwind; Dispersion:
turbulent flow around stationary and vibrating square cylinders’, Ninth MPDATA scheme (Smolarkiewicz, P. K.
Symposium on Turbulent Shear Flows, Kyoto, Japan, August 1993; and W. W. Grabowski, 1989: The
Cartesian, non-
Wall functions epsilon López, S.D. (2002) Numerische Modellierung turbulenter Sc=0.74 3 15 5 15 to 19 7 to 14 0.32 0.32 0.2 0.2 <= 1.2 3052560 multidimensional positive definite 1.00E-03 0.8 * 0.8 * 0.5
equidistant
Umströmungen von Gebäuden. PhD thesis, University of Bremen: advection transport algorithm:
Germany) ; dispersion: Reynolds-averaged advection-diffusion Nonoscillatory option. J. Compu.
equation Physics, 86, 355{375.)
Disp_005 MISKAM05mres_Goricsan modified k-e (Kato, M. and Launder, B.E. (1993) ‘The modelling of Flow: 1st order upwind; Dispersion:
turbulent flow around stationary and vibrating square cylinders’, Ninth MPDATA scheme (Smolarkiewicz, P. K.
Symposium on Turbulent Shear Flows, Kyoto, Japan, August 1993; and W. W. Grabowski, 1989: The
Cartesian, non-
Wall functions epsilon López, S.D. (2002) Numerische Modellierung turbulenter Sc=0.74 5 24 5 11 to 28 10 to 18 0.2 0.2 0.2 0.2 <= 1.2 4788000 multidimensional positive definite 1.00E-03 0.5 * 0.5 * 0.5
equidistant
Umströmungen von Gebäuden. PhD thesis, University of Bremen: advection transport algorithm:
Germany) ; dispersion: Reynolds-averaged advection-diffusion Nonoscillatory option. J. Compu.
equation Physics, 86, 355{375.)
Disp_006 MISKAM_ZAMG
Wall function? TKE epsilon Standard k-eps?, Sc=0.74?
Disp_007 Fluent_ke_Goricsan
Special non-equailibrium wall 1.7 * 1.16 *0.35 (paralell
functions, S.-E. Kim and Until residuals to container long axis /
D. Choudhury. In ASME FED Realizable k-eps by Shih et al. Computers Fluids, 24(3):227-238,
epsilon Sc=0.7 hexahedral 11//18 5 11 7//14 14//15 0.229//0.283 0.228//0.387 0.079 0.138 <= 1.3 1675712 2nd order upwind stop changing perpendicular to
1995.; dispersion: simple gradient diffusion model
Vol. 217, Separated and (~1e-5) container long axis /
Complex Flows. ASME, 1995 vertical)
Disp_008 Fluent_RSM_Goricsan
Linear pressure strain model in Fluent, (M. M. Gibson and B. E.
Launder. Ground Effects on Pressure Fluctuations in the Atmospheric
Boundary Layer. J. Fluid Mech., 86:491-511, 1978., S. Fu, B. E. 1.7 * 1.16 *0.35 (paralell
Non-equilibrium wall-function, Launder, and M. A. Leschziner. Modeling Strongly Swirling Until residuals to container long axis /
Wall BC from k, wall reflection epsilon Recirculating Jet Flow with Reynolds-Stress Transport Closures. In Sc=0.7 hexahedral 11//18 5 11 7//14 14//15 0.229//0.283 0.228//0.387 0.079 0.138 <= 1.3 1675712 2nd order upwind stop changing perpendicular to
effects Sixth Symposium on Turbulent Shear Flows, Toulouse, France, 1987., (~1e-5) container long axis /
B. E. Launder. Second-Moment Closure and Its Use in Modeling vertical)
Turbulent Industrial Flows. International Journal for Numerical
Methods in Fluids, 9:963-985, 1989.,B. E. Launder. Second-Moment
Closure: Present... and Future? Inter. J. Heat Fluid Flow, 10(4):282-
300, 1989.) ; dispersion: simple gradient diffusion model
Disp_009 FLUENTske_DiSabatino
Standard wall functions epsilon Standard k-eps, Sc=0,7 Sc=0.7 hexahedral 12 2 13 13 8 0.08 0.08 0.16 0.08 <=1.3 ~1.300.000 2nd order upwind 0.000001 0.5 * 0.5 * 0.5
Disp_010 FLUENT_Santiago
Standard wall functions epsilon Standard k-eps. Simple gradient diffusion model with Sc=0.9 Sc=0.9 0.89*1.98*0.35
Disp_011 Fluent_mskespudf_Franke Volume source in cell
epsilon Standard k-eps. Simple gradient diffusion model with Sc=0.7. Sc=0.7 containing the exp.
Rough wall-functions (Cs = 1.0) source center
Disp_012 CFX-unstr-ke_fine_Fotios Unstructured 1e-4, MAX
Volume source in cell
Standard wall functions epsilon Standard k-eps. Simple gradient diffusion model with Sc=? Sc=0.77 ~20 ~12 ~12 ~20 ~20 0.15 0.15 0.15 0.15 1.2 5500000 containing the exp.
grid residuals
source center
Disp_013 FINFLO_Hellsten1
See sheet ”Info_Flow45” cell AA21. Simple gradient diffusion model Block Third-order upwind biased scheme for Until residuals
Standard wall functions omega Sc=0.8 24 8 12 16 12 0.125 0.125 0.0833 0.0833
with Sc=0.8. structured fluxes stop decreasing
1.16 3599616
Disp_014 FINFLO_Hellsten2
See sheet ”Info_Flow45” cell AA22. Simple gradient diffusion model Block Third-order upwind biased scheme for Until residuals
Standard wall functions omega Sc=0.8 12 4 6 8 6 0.25 0.25 0.167 0.167 449952
with Sc=0.8. structured fluxes stop decreasing
1.16
Disp_015 FINFLO_Hellsten3
See sheet ”Info_Flow45” cell AA23. Simple gradient diffusion model Block Third-order upwind biased scheme for Until residuals
Standard wall functions omega Sc=0.8 6 2 3 4 3 0.5 0.5 0.333 0.333 1.34 56244
with Sc=0.8. structured fluxes stop decreasing
Disp_016 M2UE_Nuterman_Baklanov
Wall function TKE epsilon Standard k-eps. Simple gradient diffusion model with Sc=0.5. Sc=0.5 Cartesian ~10 ~5 ~10 ~10 ~5 1.29 1.58 0.74 0.25 1466828 2nd order MLU 0.001 1.2 * 1.2 * 0.25
Disp_017 VADIS_Costa_2m 0.01 reached,
Wall functions epsilon Standard k-eps, Lagrangian dispersion model, Sc=0.7 Sc=0.7 Cartesian 6 1 1 8 2 0.787 0.787 0.787 0.787 157000 2nd order upwind 0.5 * 0.5 * 0.3
0.001 prescribed
Disp_018 VADIS_Costa_1m 0.01 reached,
Wall functions epsilon Standard k-eps, Lagrangian dispersion model, Sc=0.7 Sc=0.7 Cartesian 12 2 2 16 4 0.394 0.394 0.394 0.394 3675000 2nd order upwind 0.5 * 0.5 * 0.3
0.001 prescribed
Disp_019 VADIS_Costa_0_5m 0.01 reached,
Wall functions epsilon Standard k-eps, Lagrangian dispersion model, Sc=0.7 Sc=0.7 Cartesian 24 4 4 32 8 0.197 0.197 0.197 0.197 29400000 2nd order upwind 0.5 * 0.5 * 0.3
0.001 prescribed
Disp_020 STARCD_fine_Brzozowski
Wall functions epsilon Standard k-eps. Simple gradient diffusion model with Sc=0.9 Sc=0.9
Disp_025 ADREA_Bartzis Irregular surface with
0.0001 (0.001 for
area 0.442 m^2 inside a
See sheet ”Info_Flow45” cell AA31. Simple gradient diffusion model turbulence and
Special surface-layer functions zeta (zeta=eps/(k^1.5)) Sc=0.74 Cartesian 4//5 2 8 10 5 0.48 1.2//0.96 0.277 0.125 <= 1.1 551936 1st order upwind cell of dimensions (dx =
with Sc=0.74. 0.00000001 for
1.1983m, dy = 2.4982m,
concentration)
dz = 0.3175m)
Disp_022 LASAT_ZAMG
Disp_023 Code_Saturne
epsilon Standard k-eps. Simple gradient diffusion model with Sc=?.
Rough wall-functions
Disp_024 LASAT_ZAMG_MISKAMwind
-45 degree flow case. Non-CFD model parameters c31ca3c1-0699-4a66-bc89-761c976ee739.xls ! Info_Disp_nonCFD 11/17/2011
Roughness
Run_ID Short Name Met. parameters Treatment of buildings
length
DiNo_001 ESCAPE_FMI Wind speed and direction at a
given height, a stability parameter
(e.g. Monin-Obukhov length, 0.1*Hcontainer Non-obstacle resolving
Richardson number...),
temperature, humidity.
DiNo_002 ADMS_DiSabatino Non-obstacle resolving. 1) The area
occupied by the buildings is replaced by a
single value of surface roughness
z0=0.269m, calculated by morphometric
0.269m (in the
method proposed by Macdonald, R.,
area occupied by
Wind speed and direction at a Griffiths, R., and Hall, D. (1998) ‘An
the buildings)
given height, Monin-Obukhov improved method for estimation of
0.017m (in the
length, boundary layer height. surface roughness of obstacle arrays’,
area upwind of the
Atmospheric Environment 32,
buildings)
pp.1857–1864.
2) The same z0 as in wind tunnel
experiments is used in the area upwind of
the buildings.
DiNo_003 ADMSurban_Marina 0.381 Non-obstacle resolving
DiNo_004 ADMS_ZAMG
Wind speed and direction at a parameterization of cavity zone for one
0.1
given height, a stability parameter 'effective' building
DiNo_005 OML_NERI1 u * =0.521 m/s; u * /u ref =0.076;
Modelled by roughness (roughness
Heat flux=0. Uref calc. from log
0.037 estimated at source, not representative
profile at z=7.29m and local Zo
for the plume)
and U*
DiNo_006 OML_NERI2 z 0 =0.3m; u * =0.812m/s; u * /u ref
Modelled by representative roughness,
=0.125; Heat Flux=0. Uref calc.
0.3 estimated in middle of building array
from log profile at z=7.29m and
(realistic run)
local Zo and U*
DiNo_007 CALPUFF_Krajcovicova Diagnostic wind field model
CALMET based on wind speed building area: 0.1
Non-obstacle resolving
and direction at a given height, a outside: 0.02
stability parameter