A High Elevation Aerosol Inlet Modeling Study and Inter-comparison A. Gannet Hallar 1, Ian McCubbin 1, Igor Novosselov 2, Riley Gorder 2, John Ogren 3.

Slides:



Advertisements
Similar presentations
Fluid Mechanics Research Group Two phase modelling for industrial applications Prof A.E.Holdø & R.K.Calay.
Advertisements

Extra Large Telescope Wind Engineering. Wind and Large Optical Telescopes Wind is a key factor in the design of large telescopes: larger wind-induced.
Bridging the Gap Between Statistics and Engineering Statistical calibration of CFD simulations in Urban street canyons with Experimental data Liora Malki-Epshtein.
The analysis of the two dimensional subsonic flow over a NACA 0012 airfoil using OpenFoam is presented. 1) Create the geometry and the flap Sequence of.
Coupling a Network HVAC Model to a Computational Fluid Dynamics Model Using Large Eddy Simulation Jason Floyd Hughes Associates, Inc Fire + Evacuation.
University of Western Ontario
© 2014 Pearson Education, Inc. Chapter 5 Lecture Basic Chemistry Fourth Edition Chapter 5 Electronic Structure and Periodic Trends 5.1 Electromagnetic.
Gaseous And Particulate Dispersion In Street Canyons
Current and Resistance
Lecture Objectives -Finish with modeling of PM -Discuss -Advance discretization -Specific class of problems -Discuss the CFD software.
OpenFOAM for Air Quality Ernst Meijer and Ivo Kalkman First Dutch OpenFOAM Seminar Delft, 4 november 2010.
NNMREC Arshiya Hoseyni Chime Advisor: Professor Phil Malte UW –NNMREC 04 November 2012.
MUTAC Review April 6-7, 2009, FNAL, Batavia, IL Mercury Jet Target Simulations Roman Samulyak, Wurigen Bo Applied Mathematics Department, Stony Brook University.
Using for Pollutant Dispersion Andrea Vignaroli – University of Perugia.
Evan Greer, Mentor: Dr. Marcelo Kobayashi, HARP REU Program August 2, 2012 Contact: globalwindgroup.com.
Measuring segregation of inertial particles in turbulent flows by a Full Lagrangian approach E. Meneguz Ph.D. project: Rain in a box of turbulence Supervisor:
2006 GSK Mathematical Modeling Symposium Modelling Particle Flow Dynamics Using Discrete Element Methods Mark Palmer, Valeriu Damian-Iordache, Pankaj DoshiRob.
Mark Claywell & Donald Horkheimer University of Minnesota
A Lagrangian approach to droplet condensation in turbulent clouds Rutger IJzermans, Michael W. Reeks School of Mechanical & Systems Engineering Newcastle.
fluidyn – PANAIR Fluidyn-PANAIR
Wave Nature of Light and Quantum Theory
1 CFD Analysis Process. 2 1.Formulate the Flow Problem 2.Model the Geometry 3.Model the Flow (Computational) Domain 4.Generate the Grid 5.Specify the.
Lecture Objectives: Review discretization methods for advection diffusion equation Accuracy Numerical Stability Unsteady-state CFD Explicit vs. Implicit.
Mechanistic Modeling and CFD Simulations of Oil-Water Dispersions in Separation Components Mechanistic Modeling and CFD Simulations of Oil-Water Dispersions.
ICHS4, San Francisco, September E. Papanikolaou, D. Baraldi Joint Research Centre - Institute for Energy and Transport
1 Institute for Fluid Mechanics and Heat Transfer Conex mid-term meeting, Oct 28th 2004, Warsaw 1 Numerical simulation of the flow in an experimental device.
Hiromasa Nakayama*, Klara Jurcakova** and Haruyasu Nagai*
MAE 3241: AERODYNAMICS AND FLIGHT MECHANICS
© 2011 Autodesk Freely licensed for use by educational institutions. Reuse and changes require a note indicating that content has been modified from the.
School of Aerospace Engineering MITE Numerical Modeling of Compressor and Combustor Flows Suresh Menon, Lakshmi N. Sankar Won Wook Kim S. Pannala, S.
1 Numerical study of the thermal behavior of an Nb 3 Sn high field magnet in He II Slawomir PIETROWICZ, Bertrand BAUDOUY CEA Saclay Irfu, SACM Gif-sur-Yvette.
SIMULATION OF DUST DEVILS Zhaolin GU, PhD, Professor Xi’an Jiaotong University October, 2006, CCFD Forum, Tokyo University.
UNIVERSITY OF LEEDS Aerobiological Simulations Using Arc 1 Dr Cath Noakes; Dr Andy Sleigh; Dr Carl Gilkeson; Dr Miller Camargo-Valero; Dr Amir Khan.
4. Atmospheric chemical transport models 4.1 Introduction 4.2 Box model 4.3 Three dimensional atmospheric chemical transport model.
ERT 206/4 THERMODYNAMICS SEM 2 (2011/2012). light Energy can exist in numerous forms: Thermal Mechanical Kinetic Potential Electric Magnetic Chemical.
CFX-10 Introduction Lecture 1.
Lecture Objectives -Finish with age of air modeling -Introduce particle dynamics modeling -Analyze some examples related to natural ventilation.
George Angeli 26 November, 2001 What Do We Need to Know about Wind for GSMT?
Compressor Cascade Pressure Rise Prediction
Adaptive Optics in the VLT and ELT era Atmospheric Turbulence
Ocean Surface Current Observations in PWS Carter Ohlmann Institute for Computational Earth System Science, University of California, Santa Barbara, CA.
Types of Models Marti Blad Northern Arizona University College of Engineering & Technology.
Understanding Aerosol Measurements. Purpose: Looking for Relationships  Between Aerosols and –Temperature –Cloud cover –Humidity –Precipitation –Seasonal.
ERMSAR 2012, Cologne, Germany, March 21 – 23, 2012 Aerosol Retention in Containment Leak Paths: Indications for a Code Model in the Light of COLIMA Experimental.
Brookhaven Science Associates U.S. Department of Energy MERIT Project Review December 12, 2005, BNL, Upton NY MHD Studies of Mercury Jet Target Roman Samulyak.
Modeling. How Do we Address Aerosol-Cloud Interactions? The Scale Problem Process Models ~ 10s km Mesoscale Models Cloud resolving Models Regional Models.
Enrico Da Riva (EN/CV/PJ)
ERT 206/4 THERMODYNAMICS SEM 2 (2011/2012). light Energy can exist in numerous forms: Thermal Mechanical Kinetic Potential Electric Magnetic Chemical.
2011 DSMC Workshop Workshop 2011 DSMC Workshop Workshop William McDoniel Modeling Gas and Dust Flow in Io’s Pele Plume William McDoniel D. B. Goldstein,
Lecture Objectives Review wall functions Discuss: Project 1, HW2, and HW3 Project topics.
Heat Transfer Su Yongkang School of Mechanical Engineering # 1 HEAT TRANSFER CHAPTER 7 External flow.
4. Sampling and Measurement of Concentration
Indian Institute of Space Science and Technology STUDY OF EFFECT OF GAS INJECTION OVER A TORPEDO ON FLOW-FIELD USING CFD.
2. WRF model configuration and initial conditions  Three sets of initial and lateral boundary conditions for Katrina are used, including the output from.
Technological/Societal Impact (1)SEM images of Silicon films deposited in pulsed laser ablation in vacuum Courtesy of A. Perrone Fluence of 3.0 J/cm^2.
Hindcasted wave dynamic during the passage of typhoons
Dispersion of Air Pollution and Penetration into the Local Environment
Project 8: Development and Validation of Bleed Models for Control of Supersonic Shock-Wave Interactions with Boundary Layers.
Lecture Objectives Learn about particle dynamics modeling
Study of ducted fans interference for copter type multirotor UAV/RPAS
The application of an atmospheric boundary layer to evaluate truck aerodynamics in CFD “A solution for a real-world engineering problem” Ir. Niek van.
Models of atmospheric chemistry
UAV Electronics Cooling System
COMPUTATIONAL MODELING OF PARTICLE TRANSPORT IN TURBULENT AIRFLOW
Lecture Objectives Review for exam Discuss midterm project
E. Papanikolaou, D. Baraldi
DOWNSTREAM PROCESSING CHROMATOGRAPHIC PROCESS
Lecture Objectives Ventilation Effectiveness, Thermal Comfort, and other CFD results representation Surface Radiation Models Particle modeling.
Air-conditioner -IDU Air-conditioner 2D Simplified model for Analysis.
Lecture 16 Multiphase flows Part 1.
Presentation transcript:

A High Elevation Aerosol Inlet Modeling Study and Inter-comparison A. Gannet Hallar 1, Ian McCubbin 1, Igor Novosselov 2, Riley Gorder 2, John Ogren 3 1: DRI – Storm Peak Laboratory 2: Enertechnix, Inc. 3: NOAA-ESRL-GMDL o Numerical wind tunnel : inlet 1m x 1m o Total in wind tunnel ~ 5,000,000 cells o Wind speeds: m/s o Particle sizes: 10nm – 20micron Computational Domain DRI - SPL Modeling of Current Inlets lpm DRI - Storm Peak Laboratory, CO NOAA, DOE ARM networks multiple locations Jungfraujoch Typical sampling rate 200 lpm Effects of Wind Speed and Particle Size. NOAA Jungfraujoch Factors in Sampling Efficiency η sampling = η aspiration * η transmission Aspiration efficiency related to isokinetic sampling (velocity mismatch, sampling orientation), free stream turbulence Transmission efficiency – internal losses due to: inertial impaction, turbulent dispersion, gravitational settling, electrostatic interaction Abstract - A51A This study presents a comparison of three high volume aerosol inlets used for atmospheric sampling at various sites, including the Desert Research Institute’s Storm Peak Laboratory, the Sphinx Laboratory at Jungfraujoch (Switzerland), and the design commonly used by NOAA’s Global Monitoring Division and the Department of Energy’s Atmospheric Radiation Measurement Program. The inlets are compared using CFD analysis over a range of wind speeds of m/s and sampling flow rate of 1000 liter per minute (lpm). The simulations were performed in 3-dimensional numerical wind tunnel. Two different turbulence models: k-epsilon and detached eddy simulations were used, and the effects of particle – turbulence coupling were examined. The transmission efficiencies for these inlets were evaluated for particles of 10 nm-20um diameter. The modeling results show that for all three inlets transmission decreases with increase of particle size due to particle inertial impaction on the inner walls of the inlets. Additionally, the transmission efficiency decreases at higher wind speeds due to the formation of the strong recirculation zone inside the inlet geometry. DRI Storm Peak and Jungfraujoch inlet efficiencies were found similar for over the range of wind speed and particle sizes. The NOAA inlet was found to have the highest sampling efficiency but was the most sensitive to wind speed, due to its high internal volume. The choice of turbulent dispersion model significantly influences modeling results, especially for high internal volume of the NOAA inlet. Flow field is solved in a numerical wind tunnel for external flow (Eulerian system) Transient Detached Numerical Simulation (DES) realizable k-  wall treatment Second order numerical convergence scheme Wind speed varied - Inlet sampling rate is constant – 1000 lpm Simulations Flow field: Velocity 2.5 m/s wind 15 m/s wind Particle trajectories Efficiency calculation includes gravitational, inertial, turbulent dispersion losses: η inlet = # particles transmitted / # massless particles transmitted Particles are introduced upstream of the inlet (Lagrangian tracking) No bounce boundary condition (particle stick if hit the wall) Turbulent dispersion – Discrete Random Walk (DRW) with random eddy life time DRW Model validation (external flow) Lowest penetration of larger particles Flow is well-structured DRI inlet Particle Tracks 3D vortex formation at the higher wind speeds Sampling on the symmetry plane NOAA inlet Particle Tracks Low penetration of larger particles Low turbulent dispersion losses NOTE: Simulations were done with a sample flowrate that was 5-6 times greater than in normal operation Jungfraujoch inlet Particle Tracks 10 m/s wind Blue - 1 um Light blue–10 um Red -20 um Blue - 1 um Light blue–10 um Red -20 um Inlet comparison The transmission efficiencies decrease with increasing particle size Sensitivity to wind speed due to formation of large eddies at higher wind speeds Blue - 1 um Light blue–10 um Red -20 um 10 m/s wind New Design of SPL Inlet m/s Slotted entrance to re-direct the flow upwards Internal vanes to limit eddy formation