A study of heat transfer effects on air pollution dispersion in street canyons by numerical simulations

Similar documents
URBAN ENERGY AND MICROCLIMATE: WIND TUNNEL EXPERIMENTS AND MULTISCALE MODELING

Air Flow Exchange Velocity of Urban Canyon Cavities due to Thermal Spatial Differences

Numerical simulation of topographic effects on wind flow fields over complex terrain

DUE TO EXTERNAL FORCES

Surrounding buildings and wind pressure distribution on a high rise building

AIRFLOW GENERATION IN A TUNNEL USING A SACCARDO VENTILATION SYSTEM AGAINST THE BUOYANCY EFFECT PRODUCED BY A FIRE

COMPUTATIONAL FLOW MODEL OF WESTFALL'S LEADING TAB FLOW CONDITIONER AGM-09-R-08 Rev. B. By Kimbal A. Hall, PE

Wind tunnel test and numerical simulation of wind pressure on a high-rise building

COMPARISONS OF COMPUTATIONAL FLUID DYNAMICS AND

Influence of rounding corners on unsteady flow and heat transfer around a square cylinder

A Numerical Study of Thermal Effects on Flow and Pollutant Dispersion in Urban Street Canyons

Numerical Investigation of Multi Airfoil Effect on Performance Increase of Wind Turbine

Wind pressure coefficient determination for greenhouses built in a reclaimed land using CFD technique

AIR POLLUTION DISPERSION INSIDE A STREET CANYON OF GÖTTINGER STRASSE (HANNOVER, GERMANY) NEW RESULTS OF THE ANALYSIS OF FULL SCALE DATA

a high-rise (78 m) building in the city of Antwerp. CFD simulations are performed for the building with and without second-skin facade concept impleme

Numerical Analysis of Wind loads on Tapered Shape Tall Buildings

Pressure coefficient on flat roofs of rectangular buildings

6.28 PREDICTION OF FOG EPISODES AT THE AIRPORT OF MADRID- BARAJAS USING DIFFERENT MODELING APPROACHES

Aerodynamic Performance of Trains with Different Longitudinal Section Lines under Crosswind

5.22 EVALUATION OF TURBULENCE FROM TRAFFIC USING EXPERIMENTAL DATA OBTAINED IN A STREET CANYON

The Effect of Urban Geometries and Roof Shapes on Airflow and Pollutant Dispersion: A CFD Investigation. Hui Wen

Validating CFD Simulation Results: Wind flow around a surface mounted cube in a turbulent channel flow

Investigations on the Aerodynamic Forces of 2-D Square Lattice Tower Section Using CFD

High Swept-back Delta Wing Flow

Quantification of the Effects of Turbulence in Wind on the Flutter Stability of Suspension Bridges

Unsteady Aerodynamics of Tandem Airfoils Pitching in Phase

THE EFFECT OF LEADING AND TRAILING EDGE PROTUBERANCES ON AEROFOIL PERFORMANCE

Injector Dynamics Assumptions and their Impact on Predicting Cavitation and Performance

The Usage of Propeller Tunnels For Higher Efficiency and Lower Vibration. M. Burak Şamşul

AE Dept., KFUPM. Dr. Abdullah M. Al-Garni. Fuel Economy. Emissions Maximum Speed Acceleration Directional Stability Stability.

Geophysical Fluid Dynamics of the Earth. Jeffrey B. Weiss University of Colorado, Boulder

Numerical Simulations of Two-Phase Flow in a Dorr-Oliver Flotation Cell Model

Full scale measurements and simulations of the wind speed in the close proximity of the building skin

Measurement and simulation of the flow field around a triangular lattice meteorological mast

MODELING AND SIMULATION OF VALVE COEFFICIENTS AND CAVITATION CHARACTERISTICS IN A BALL VALVE

CFD ANALYSIS AND COMPARISON USING ANSYS AND STAR-CCM+ OF MODEL AEROFOIL SELIG 1223

Improving pedestrian wind comfort around a high rise building in an urban area: a case study by CFD simulations and on-site measurements

Analysis on Turbulent Flows using Large-eddy Simulation on the Seaside Complex Terrain

The effect of back spin on a table tennis ball moving in a viscous fluid.

Wind tunnel tests of a non-typical stadium roof

Numerical prediction of air flow within street canyons based on different two-equation k-ε models

CFD Analysis ofwind Turbine Airfoil at Various Angles of Attack

CFD and Physical Modeling of DSI/ACI Distribution

The evolution of the application of CFD on pedestrian wind comfort in engineering practice, a validation study

APPLICATION OF COMPUTATIONAL FLUID DYNAMICS (CFD) IN WIND ANALYSIS OF TALL BUILDINGS. Damith Mohotti, Priyan Mendis, Tuan Ngo

Effect of Diameter on the Aerodynamics of Sepaktakraw Balls, A Computational Study

Journal of Engineering Science and Technology Review 9 (5) (2016) Research Article. CFD Simulations of Flow Around Octagonal Shaped Structures

External Pressure Coefficients on Saw-tooth and Mono-sloped Roofs

Numerical analysis of surface pressure coefficients for a building with balconies

A Study on the Effects of Wind on the Drift Loss of a Cooling Tower

Lecture 7. More on BL wind profiles and turbulent eddy structures. In this lecture

REVIEW Effects of Side Vents and Span Numbers on Wind-Induced Natural Ventilation of a Gothic Multi-Span Greenhouse

Determination of the wind pressure distribution on the facade of the triangularly shaped high-rise building structure

2 Asymptotic speed deficit from boundary layer considerations

CFD analysis & Experimental Investigation of Shell & Tube Type Heat Exchanger with modified Slotted Baffles

Investigation of Suction Process of Scroll Compressors

Static Extended Trailing Edge for Lift Enhancement: Experimental and Computational Studies

10.6 The Dynamics of Drainage Flows Developed on a Low Angle Slope in a Large Valley Sharon Zhong 1 and C. David Whiteman 2

Aerodynamic Shape Design of the Bow Network Monitoring Equipment of High-speed Train

Modelling the Output of a Flat-Roof Mounted Wind Turbine with an Edge Mounted Lip

Results and Discussion for Steady Measurements

Air Craft Winglet Design and Performance: Cant Angle Effect

J. Szantyr Lecture No. 21 Aerodynamics of the lifting foils Lifting foils are important parts of many products of contemporary technology.

Application of Simulation Technology to Mitsubishi Air Lubrication System

Experimental Investigation Of Flow Past A Rough Surfaced Cylinder

Atmospheric Boundary Layer Simulation Using Wall Function Approach in OpenFoam CFD Software

NUMERICAL SIMULATION OF WIND INTERFERENCE EFFECT

Wake modelling for offshore wind turbine parks. Jens N. Sørensen Department of Wind Energy Technical University of Denmark

Workshop 1: Bubbly Flow in a Rectangular Bubble Column. Multiphase Flow Modeling In ANSYS CFX Release ANSYS, Inc. WS1-1 Release 14.

Roof Mounted Wind Turbines: A Methodology for Assessing Potential Roof Mounting Locations

Wind Effect on Smoke Exhaust by Natural Vent

Numerical Simulation And Aerodynamic Performance Comparison Between Seagull Aerofoil and NACA 4412 Aerofoil under Low-Reynolds 1

AERODYNAMIC CHARACTERISTICS OF SPIN PHENOMENON FOR DELTA WING

Computational evaluation of pedestrian wind comfort and wind safety around a high-rise building in an urban area

THREE DIMENSIONAL STRUCTURES OF FLOW BEHIND A

EFFECTS OF SIDEWALL OPENINGS ON THE WIND LOADS ON PIPE-FRAMED GREENHOUSES

NUMERICAL SIMULATION OF ACTIVE FLOW CONTROL BASED ON STREAMWISE VORTICES FOR A BLUNT TRAILING EDGE AIRFOIL

AERODYNAMIC CHARACTERISTICS OF NACA 0012 AIRFOIL SECTION AT DIFFERENT ANGLES OF ATTACK

Energy from wind and water extracted by Horizontal Axis Turbine

CYCLE ANALYSIS OF LINEAR COMPRESSORS USING THREE- DIMENSIONAL CFD

Computational Analysis of the S Airfoil Aerodynamic Performance

SUMMARY OF THE EXPERIMENTAL STUDIES OF COLD HELIUM PROPAGATION ALONG A SCALE MODEL OF THE LHC TUNNEL

Transitional Steps Zone in Steeply Sloping Stepped Spillways

Exploring wave-turbulence interaction through LES modeling

Wind Flow Model of Area Surrounding the Case Western Reserve University Wind Turbine

CFD Study of Solid Wind Tunnel Wall Effects on Wing Characteristics

WIND AFFECTED ISOTHERMAL AIRFLOW PATTERNS IN A SCALE MODEL OF A SWINE BARN MEASURED WITH PIV SYSTEM

Senior mechanical energy conversion trends

EXPERIMENTAL AND NUMERICAL STUDY OF A TWO- ELEMENT WING WITH GURNEY FLAP

Computer Simulation of a Train Exiting a Tunnel through a Varying Crosswind

PERFORMANCE OF A FLAPPED DUCT EXHAUSTING INTO A COMPRESSIBLE EXTERNAL FLOW

CFD Analysis and Wind Tunnel Experiment on a Typical Launch Vehicle Model

Aerodynamic Analysis of Blended Winglet for Low Speed Aircraft

Flow and Mixing in the Liquid between Bubbles

Design & Analysis of Natural Laminar Flow Supercritical Aerofoil for Increasing L/D Ratio Using Gurney Flap

Numerical Simulation of Wind Effect on a Rooftop Solar Array

arxiv: v1 [physics.flu-dyn] 27 Mar 2017

Study on wind turbine arrangement for offshore wind farms

International Journal of Technical Research and Applications e-issn: , Volume 4, Issue 3 (May-June, 2016), PP.

AN IMPROVED CROSS VENTILATION MODEL IN WINDY REGIONS

Transcription:

A study of heat transfer effects on air pollution dispersion in street canyons by numerical simulations N. Moussiopoulos, I. Ossanlis and Ph. Barmpas Aristotle University Thessaloniki, Greece

MIMO 3D, prognostic microscale model. Predicts air motion near building structures. Solves conservation equations for: Mass Momentum Scalar quantities like potential temperature, TKE & specific humidity Heating module calculates heat transfer through: Conduction Convection Radiation

MIMO validation (1/3) vs. wind tunnel experiments of Rafailidis (1997) for the isothermal case (cf. Assimakopoulos, 2001) vs. field measurements of Panskus et.al. (2002) for the heated walls case vs. wind tunnel experiments of Bezpalcová (2003) for pollutants dispersion.

MIMO validation (2/3) Windward wall heated case Isothermal T = 80K T = 120K Isothermal T = 80K T = 120K MIMO model results Field measurements results

MIMO validation (3/3) Pollutant dispersion case Wind tunnel results MIMO model results

Current study Effect of heated street canyon walls on the dispersion of pollutants is considered. Heat transfer from the street canyon walls to the air through convection based on the heat transfer coefficient α. Heat transfer coefficient α calculated by: α = ( T T ) ( T T ) 0 Q f = ρc 0 p u θ u * is the friction velocity θ * is the surface layer temperature scale * *

Simulations in 2D were performed for street canyons with aspect ratios of 0.33, 1.0 & 2.0 For all aspect ratios: Either the leeward or the windward wall was heated T between heated wall and ambient air assumed at: a) 0 K (Isothermal case) b) 5 K c) 10 K d) 15 K Current discussion focuses on the isothermal case and the cases of (leeward or windward) heating by 15K Results of MIMO compared with those of TASCflow.

Assumed boundary conditions: Inlet power law wind profile with U δ =5 m/s Surface layer height δ = 100 m Roughness length z o = 0.05m Inflow turbulence intensity = 0.03 Mass flow of passive pollutants Qs = 1.5mg/s Turbulence model: standard k-ε with standard wall functions

Same computational domain used for all cases Inlet conditions 5H Grid size Symmetry conditions Wall conditions W Aspect ratio 0.33 142 115 cells H Aspect ratio 1.0 167 115 cells Aspect ratio 2.0 207 115 cells 9H δ Free outlet

Results obtained for In-street canyon flow & concentration field Calculated concentration across the street canyon at Y/H 0.15, 0.5 & 1.0 Non dimensional values of the calculated concentration obtained: ( Q L) C = CU H / s / * δ C* is the non-dimensional concentration C is the calculated inert pollutant concentration U δ is the reference wind velocity H is the height of the street canyon Q s is the mass flow of the passive pollutants L is the characteristic length of the source

Aspect ratio 0.33, isothermal case MIMO predicts a system of two counter rotating vortices. TASCflow predicts a system of three vortices with adjacent ones rotating in opposite directions. MIMO: maximum concentrations near the windward side TASCflow: maximum concentrations near the leeward side

Flow field comparison for aspect ratio 0.33 for the isothermal case (a) MIMO (b) TASCflow

Aspect ratio 0.33, leeward wall heated ( Τ = 15Κ) Both codes predict a system of three vortices: One large primary vortex Two small ones at the lower part of the street canyon Disagreement between MIMO & TASCflow regarding the size of the vortices: MIMO predicts a much smaller vortex near the leeward wall side than TASCflow MIMO: relatively equal concentrations near the two wall sides TASCflow: maximum concentration near the windward wall side

Flow field comparison for aspect ratio 0.33 with the leeward wall heated, for Τ = 15Κ (a) MIMO (b) TASCflow

Aspect ratio 0.33, windward wall heated ( Τ = 15Κ) MIMO predicts a system of three vortices: One vortex near the roof level One large, centrally located vortex One small at the lower part of the street canyon TASCflow predicts a system of two counter rotating vortices: One near the roof level One large vortex covering 75% of the total street canyon area MIMO: maximum concentrations near the leeward side while TASCflow near the windward side

Flow field comparison for aspect ratio 0.33 with the windward wall heated, for Τ = 15Κ (a) MIMO (b) TASCflow

C* Calculated dimensionless concentration across the street canyon for aspect ratio 0.33 (a) Y/H=0.15 MIMO TASCflow 2000 1800 1600 1400 1200 1000 800 600 400 200 0 0.0 0.2 0.4 0.6 0.8 1.0 1.2 X/W

C* Calculated dimensionless concentration across the street canyon for aspect ratio 0.33 1000 900 800 700 600 500 400 300 200 100 0 (b) Y/H=0.5 MIMO TASCflow 0.0 0.2 0.4 0.6 0.8 1.0 1.2 X/W

C* Calculated dimensionless concentration across the street canyon for aspect ratio 0.33 140 120 100 80 60 40 20 0 (c) Y/H=1.0 MIMO TASCflow 0.0 0.2 0.4 0.6 0.8 1.0 1.2 X/W

Aspect ratio 1.0 The flow fields predicted by both codes are in good agreement One centrally located vortex Two small ones at the street canyon ground level near each of the building walls For all cases for Y/H 0.5, both codes predict maximum concentrations near the leeward side For Y/H = 1.0 both codes predict maximum concentrations near the windward side Heat transfer phenomena do not affect markedly the flow field Calculated concentrations increase when either the leeward or the windward wall is heated

Flow field comparison for aspect ratio 1.0 for the isothermal case (a) MIMO (b) TASCflow

C* Calculated dimensionless concentration across the street canyon for aspect ratio 1.0 2000 1800 1600 1400 1200 1000 800 600 400 200 0 (a) Y/H=0.15 MIMO TASCflow 0.0 0.2 0.4 0.6 0.8 1.0 1.2 X/W

C* Calculated dimensionless concentration across the street canyon for aspect ratio 1.0 1400 1200 1000 800 600 400 200 0 (b) Y/H=0.5 MIMO TASCflow 0.0 0.2 0.4 0.6 0.8 1.0 1.2 X/W

C* Calculated dimensionless concentration across the street canyon for aspect ratio 1.0 400 350 300 250 200 150 100 50 0 (c) Y/H=1.0 MIMO TASCflow 0.0 0.2 0.4 0.6 0.8 1.0 1.2 X/W

Aspect ratio 2.0 For aspect ratio 2.0 the flow fields predicted by both codes are in good agreement One centrally located vortex Two small ones at the street canyon ground level near each of the building walls TASCflow however, predicts a larger vortex near the leeward wall side than MIMO As a result for Y/H 0.5, for all cases MIMO predicts maximum concentrations near the leeward wall side at X/W 0.1 while TASCflow at X/W 0.3 Heat transfer phenomena do not affect markedly the flow field Calculated concentrations increase when either the leeward or the windward wall is heated

Flow field comparison for aspect ratio 2.0 for the isothermal case (a) MIMO (b) TASCflow

Calculated dimensionless concentration across the street canyon for aspect ratio 2.0 C* (a) Y/H=0.15 MIMO TASCflow 1000 900 800 700 600 500 400 300 200 100 0 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 X/W

Calculated dimensionless concentration across the street canyon for aspect ratio 2.0 C* 700 600 500 400 300 200 100 (b) Y/H=0.5 MIMO TASCflow 0 0.0 0.2 0.4 0.6 0.8 1.0 X/W

Calculated dimensionless concentration across the street canyon for aspect ratio 2.0 C* 300 250 200 150 100 50 0 (c) Y/H=1.0 MIMO TASCflow 0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 X/W

Aspect ratios 1.0 and 2.0 Conclusions The flow field predicted by MIMO is similar to that obtained with TASCflow for all cases considered Yet, MIMO predicts higher velocity components than TASCflow and therefore there is a strong disagreement between the corresponding concentration fields Aspect ratio 0.33 Results show disagreement between the two codes in the predicted flow fields for all cases As a result, the two codes predict maximum concentrations at different regions near the building walls There is a need to study further how the selection of specific turbulence models - wall functions affects model performance.

The Guerville street canyon experiment (PICADA project)

Comparison of u & v velocity component fields respectively for aspect ratio 1.0 for the isothermal case MIMO TASCflow v-component u-component

Comparison of u & v velocity component fields respectively for aspect ratio 2.0 for the isothermal case MIMO TASCflow v-component u-component