DESIGN ISSUES OF A NEW WIND TUNNEL LABORATORY FOR ENVIRONMENTAL AND VEHICLE AERODYNAMICS. Márton BALCZÓ PhD, assistant professor

Similar documents
NanoShine Group Corp.

Innovation Days Efficient Dynamics. Energy and Environmental Test Centre.

EFFECT OF SURFACE ROUGHNESS ON PERFORMANCE OF WIND TURBINE

17/11/2016. Turbomachinery & Heat Transfer Laboratory Faculty of Aerospace Engineering Technion Israel Institute of Technology, Israel

PM/BC situation in Hungary and measures for its reduction

ENGINE STARTING PERFORMANCE EVALUATION AT STATIC STATE CONDITIONS USING SUPERSONIC AIR INTAKE

ABSTRACT INTRODUCTION

Transactions on Modelling and Simulation vol 10, 1995 WIT Press, ISSN X

CFD Investigation of Influence of Tube Bundle Cross-Section over Pressure Drop and Heat Transfer Rate

Vehicle Aerodynamics Subscription Development of Numerical Simulation Method of Flow Around Automobile Using Meshfree Method

Development of a probe traversing system for an open test section wind tunnel

Ground Effect and Turbulence Simulation at the Pininfarina Wind Tunnel. Giuseppe Carlino Aerodynamic and Aeroacoustic Research Center

AN EXPERIMENTAL STUDY OF THE AERODYNAMICS FORCES ACTING ON A TRUCK

Dave Bone. DREAM Project Coordinator

Chapter 1: Introduction to Automobile Aerodynamics...1

Experimental Verification of Low Emission Combustor Technology at DLR

AUTOMOTIVE TESTING AND OPTIMIZATION. Tools for designing tomorrow's vehicles

Root Cause Analysis of a vibration problem in a propylene turbo compressor. Pieter van Beek, Jan Smeulers

(1) Keywords: CFD, helicopter fuselage, main rotor, disc actuator

Aerofoil Ventilation Fans. Fantek. Quality & Performance at Affordable Prices

Gas Turbines and Aerospace Propulsion

Paper ID ICLASS EXPERIMENTAL INVESTIGATION OF SPRAY IMPINGEMENT ON A RAPIDLY ROTATING CYLINDER WALL

Foundations of Thermodynamics and Chemistry. 1 Introduction Preface Model-Building Simulation... 5 References...

The Role of the European Research Establishments in AWIATOR on examples from fligth test measurements technologies

Investigation of converging slot-hole geometry for film cooling of gas turbine blades

Field measurements and CFD simulation for wind effect on PV solar panels mounted on flat roofs

PROJECT PORTFOLIO. A list of projects completed by Sukra Helitek and their briefs Sukra Helitek 1 P a g e 33

Special Products Catalogue 2018 Visit our new website!

Automatic CFD optimisation of biomass combustion plants. Ali Shiehnejadhesar

CFD on Cavitation around Marine Propellers with Energy-Saving Devices

CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION

VIBRATION OF AUTOMOBILE SIDE VIEW MIRROR DUE TO AERODYNAMIC INPUTS

STUDY OF THE AERODYNAMIC NOISE CHARACTERISTICS OF BLUFF BODIES AS A PANTOGRAPH MEMBER

Tank mixing systems with liquid jet mixing nozzles

Airship Technology. G. A. Khoury. J. D. Gillett Formerly of Brunei University and The Airship Association CAMBRIDGE UNIVERSITY PRESS

Introduction of the research concerning exhaust gas from the vehicle entering cabin

FLIGHT TEST RESULTS AT TRANSONIC REGION ON SUPERSONIC EXPERIMENTAL AIRPLANE (NEXST-1)

Aircraft Pollution Monitoring Project

TFS 1000 EXTRACTION / FILTER / POLLUTION CONTROL // TECHNOLOGY

Guide vane for agricultural applications

Aerodynamic Design of the Reichstag

Aerodynamic Study of the Ahmed Body in Road-Situations using Computational Fluid Dynamics

WITHOUT MUCH OF A STIR

New Catalytic Stripper System for the Measurement of Solid Particle Mass, Number, and Size Emissions from Internal Combustion Engines

TUBULAR CENTRIFUGAL INLINE FANS

An Investigation into Unsteady Base Bleed for Drag Reduction in Bluff Two-Box SUV s

Review of in use factors affecting the fuel consumption and CO 2 emissions of passenger cars On going study. Brussels 9 December 2014

WIND TUNNEL TEST WITH MOVING VEHICLE MODEL FOR AERODYNAMIC FORCES OF VEHICLE-BRIDGE SYSTEMS UNDER CROSS WIND

Proposal to establish a laboratory for combustion studies

The hepia Moto2 Aerodynamic Program - From CFD to the Track

SPRAY INTERACTION AND DROPLET COALESCENCE IN TURBULENT AIR-FLOW. AN EXPERIMENTAL STUDY WITH APPLICATION TO GAS TURBINE HIGH FOGGING

Lecture 4 CFD for Bluff-Body Stabilized Flames

American Wind s Story

Wet flame-jet drilling: An alternative technique to access deep heat reservoirs

Large Low-speed Facility (LLF)

FLOW CONTROL THROUGH VORTEX SHEDDING INTERACTION OF ONE CYLINDER DOWNSTREAM OF ANOTHER. Jonathan Payton 1, and *Sam M Dakka 2

Drag Characteristics of a Pickup Truck according to the Bed Geometry

Enhanced Heat Transfer Surface Development for Exterior Tube Surfaces

FINAL REPORT MARCH 2008

COMPUTATIONAL FLOW MODEL OF WESTFALL'S 2900 MIXER TO BE USED BY CNRL FOR BITUMEN VISCOSITY CONTROL Report R0. By Kimbal A.

Energy Recovery Laboratory Exhaust

DIAGNOSTIC TESTING USING ASHRAE 110. Gerhard Knutson, Ph.D., CIH Knutson Ventilation, Inc

DESIGN AND ANALYSIS OF UNDERTRAY DIFFUSER FOR A FORMULA STYLE RACECAR

Comparison of Swirl, Turbulence Generating Devices in Compression ignition Engine

DLR s Free Piston Linear Generator FPLG Development of an Innovative Linear Power Unit

Development of a Variable Stability, Modular UAV Airframe for Local Research Purposes

Full-Scale 1903 Wright Flyer Wind Tunnel Test Results From the NASA Ames Research Center

Multidisciplinary Design Optimization of a Truss-Braced Wing Aircraft with Tip-Mounted Engines

Research and Reviews: Journal of Engineering and Technology

downflo workstation dust collectors

The Effects of Damage and Uncertainty on the Aeroelastic / Aeroservoelastic Behavior and Safety of Composite Aircraft. JAMS Meeting, May

IJSRD - International Journal for Scientific Research & Development Vol. 4, Issue 06, 2016 ISSN (online):

Test Procedure on Exhaust Gas Entering into Vehicle Cabin

Application Equipment and Techniques 1

Udvavisk. Engineering Analysis with CFD. 1st Floor (B), Tower II, Ramana Complex #322, Velachery Main Road Velachery, Chennai

Modeling, Structural & CFD Analysis and Optimization of UAV

AERODYNAMIC BICYCLE HELMET DESIGN USING A TRUNCATED AIRFOIL WITH TRAILING EDGE MODIFICATIONS

Monitoring Variable Speed Bearings Using Ultrasound

Air Flow Measurement Technologies

The Effects of Damage and Uncertainty on the Aeroelastic / Aeroservoelastic Behavior and Safety of Composite Aircraft

Results of the Blind Comparison

EFFECTS OF LOCAL AND GENERAL EXHAUST VENTILATION ON CONTROL OF CONTAMINANTS

THERMAL TO MECHANICAL ENERGY CONVERSION: ENGINES AND REQUIREMENTS Vol. I - Thermal Protection of Power Plants - B.M.Galitseyskiy

AERODYNAMIC BICYCLE HELMET DESIGN USING A TRUNCATED AIRFOIL WITH TRAILING EDGE MODIFICATIONS

Downflo workstation DuSt ColleCtorS

Smart Grids: anticipated trends and policy directions

COMPUTATIONAL ANALYSIS OF TWO DIMENSIONAL FLOWS ON A CONVERTIBLE CAR ROOF ABDULLAH B. MUHAMAD NAWI

CFD analysis on the aerodynamics characteristics of Jakarta-Bandung high speed train

MRT 300/2 MARKING REMOVAL TRUCK ENGLISH INNOVATIONS FOR POWERFUL PERFORMANCES

Aerodynamic Characteristics of Sedan with the Rolling Road Ground Effect Simulation System

Advanced Aerodynamic Design Technologies for High Performance Turbochargers

V&V Exercise for a Solar Tower Power Plant

Innovating the future of disaster relief

CONTENTS. History. Joulin s Performance. Joulin s System. Options. Questionnaire

3D In-cylinder Cold Flow Simulation Studies in an IC Engine using CFD

Analysis of External Aerodynamics of Sedan and Hatch Back Car Models Having Same Frontal Area by Experimental Wind Tunnel Method

(Class II Type A2 & B2)

The use of CFD at hepia The Swiss Team Moto2 fastest of the World Championship

Numerical Investigation of the Effect of Excess Air and Thermal Power Variation in a Liquid Fuelled Boiler

AERODYNAMIC STABILITY OF A SUPER LONG-SPAN BRIDGE WITH SLOTTED BOX GIRDER

Transcription:

DESIGN ISSUES OF A NEW WIND TUNNEL LABORATORY FOR ENVIRONMENTAL AND VEHICLE AERODYNAMICS Márton BALCZÓ PhD, assistant professor

CONTENTS 2 1. Environmental and building aerodynamics at the DFM 2. Boundary layer wind tunnels (BLWTs) 3. The existing BLWT 4. Requirements of a new laboratory 5. BLWT application matrix 6. Space and design constraints 7. Design variants 8. Summary

ENVIRONMENTAL AND BUILDING AERODYNAMICS AT THE THEODORE VON KÁRMÁN WT LAB 3 1. Large Göttingen-type wind tunnel 2. Boundary layer modelling using spikes, rods and roughness elements 3. Modell scale environmental : 1:350-1000 4. Modell scale building aerodynamics: 1:100 1:0 (turbulent length scale does not fit)

THE BOUNDARY-LAYER WIND TUNNEL 4 WT of Building Research Institute (ÉTI), rebuilt 1984 decommisioned and bought by our laboratory 03

THE EXISTING BOUNDARY-LAYER TUNNEL 5 test section type closed preparation section length [m] 5.5 Test section [m] 2.2 x 1.4 max. wind speed [m/s] 19

THE EXISTING BOUNDARY-LAYER TUNNEL 6 test section type closed preparation section length [m] 5.5 Test section [m] 2.2 x 1.4 max. wind speed [m/s] 19 Problems 1. exposure to weather 2. dust generation during operation 3. no security of valuable instrumentation 4. extreme heat under the pentice during summer. 5. lack of curtains or disillumination for flow visualisation. 6. no laser protection of trespassers. 7. use of external air causes unsteady flow.

REQUIREMENTS OF A NEW LABORATORY 7 1. Long boundary layer generation section equilibrium boundary layer (BL) larger BL thickness larger model scale 2. (at least partial) weather protection closed laboratory space QUESTIONS 1. Refurbish the existing BLWT / extend the existing BLWT / fully new BLWT? 2. use of external air (as today) / circulation of internal air / recirculating tunnel? 3. How to fit the wind tunnel into the available space?

BOUNDARY-LAYER WIND TUNNELS 8 Wind tunnel Test section power Top Owner Built Layout Size Type W speed University of Adelaide 11 closed circuit Comment / Specialities Cost [m 2 ] [m] [kw] [m/s] [ ] 31 19 closed/ open 3 6 135 33 2.75 2m high speed test section for aeronautical testing up to 50 m/s is located in the other leg. 3.65M ETH Zürich / EMPA 11 closed circuit 25 6.5 closed 1.9 110 28 Use of external air possible instead of recirculation. Test section blocks easily removable. Leibniz Institute for Agr. Eng. Potsdam 12 open return 29 6.5 closed 3 Mainly used in agricultural research, odour dispersion 1.18M TU Eindhoven ** closed circuit 42 12** closed n/a n/a n/a Facilitating building will be approx. 850 m 2 1.4M ** * flow preparation section + test section length added ** in design phase, estimated values based on [7] Conclusion: closed circuit is the preferred type

WIND TUNNELS IN HUNGARY (1) 9 Wind tunnel (WT) Built Total lengt Test section Top speed Application area Owner Type h Type Width [year] [m] [m] [m/s] Budapest closed return 1936-38 28.2 open 2.6 60 aerodynamics of vehicles, buildings, University of pollutant dispersion Technology and closed return 1936-38 10.2 open 1.4 25 drag force measurement on smaller Economics objects open return, 1984 13.6 closed 2.2 19 building and environmetal suction type aerodynamics University of Miskolc open return, suction type open return, blower type Comment / Specialties 3D probe traversing system, modular floor, 2m-turntable long flow preparation section, adjustable roof, located outside 1941 6 closed 0.5 18 anemometer calibration, flow around 3D traversing system installed bodies 13 5 open or 0.35 24 vehicle aerodynamics measurementsclosed test section can be closed removed for open jet configuration 13 5.2 open or 1 24 flow around 2D bluff bodies and equipped with 3-component force open return, blower type closed airfoils closed return 1982 13 closed 1.2 30 general fluid dynamics, boundary layer modelling open return/closed return balance isolated wind tunnel, temperature adjustable between -10 to +50 C 09 8.6 closed 0.5 30 fundamental fluid dynamics research at low speeds: closed return / high speeds: open return open return 12 6.5 open 0.4 6 turbulence, turbulence generator research 3D traversing system installed

WIND TUNNELS IN HUNGARY (2) 10 Wind tunnel (WT) Built Total lengt Test section Top speed Owner Type h Type Width [year] [m] [m] [m/s] National open return, Agricultural suction type Research and Innovation Center Szent István University Hungarian Meteorological Service University of Debrecen, Faculty of Science and Technology University of Szeged, Faculty of Science and Informatics University of Nyíregyháza open return, suction type open return, suction type open return, suction type Application area 04 13 closed 2 3 testing of agricultural spray application techniques 04 6 closed 0.5 19 calibration of anemometers 14 5.6 closed 1 25 calibration of anemometers Comment / Specialties adjustable roof, 2.5m turntable 02 6.1 closed 0.652 50 calibration of anemometers Theodor Friedrichs Co. Type 84. Min. speed 0.15 m/s closed return 1970 12.3 closed 0.8 14 soil erosion experiments eqipped with a particle filter open return blower open return or closed return 1980 12 closed 0.8 17 in-situ soil erosion experiments WT without a bottom to be placed on the investigated soil surface 12 9 closed 0.25 n/a drying research Not operational at the moment due to change of location

WIND TUNNEL APPLICATION MATRIX 11 Boundary layer wind tunnel applications open return external air internal air closed circuit building wind load measurements ++ - ++ aeroelastic testing + - ++ pollutant dispersion measurements - ++ ++ sand erosion / snow erosion / dirty measurements laser based measurement techniques ++ - + * - + ++ vehicle areodynamics + - ++ use during winter (below 0 deg) - ++ ++ cold weather testing (during winter) + - - * with switchable external air supply or separator behind the test section Conclusion an open-return tunnel is limited in application (whether with external or with internal air) Closed circuit WT more flexible

SPACE AND DESIGN CONSTRAINTS 12 1. Budapest world heritage conservation area (buffer zone) 2. Access for users of neighbouring laboratories and workshops 3. Campus promenade (limits length) DFM offices yard with WT DFM lab other faculty labs

DESIGN VARIANTS 1. Budapest world heritage conservation area (buffer zone) 2. Access for users of neighbouring laboratories and workshops 3. Campus promenade (limits length) 13 Available space: 26.5 x 11 m 5 m height

DESIGN VARIANTS 14 Version A original design Wind tunnel using external air but placed inside a closed laboratory Multiple fans to save length Optional forward test section

DESIGN VARIANTS 15 Version A outlet inlet Inlet behind screen Inlet behind screen outlet

CFD SIMULATION OF THE INLET FLOW CONDITIONS AT VERSION A 16 Excerpt of CFD simulations performed by Péter Tóth Longitudinal vortex inside the contraction caused by assymmetric inflow Reduction of vortex strength through contraction design changes

DESIGN VARIANTS 17 Version B improved design Same as A, but: Movable wind tunnel : winter operation with internal air (speed limited)

FLOW FIELD WITH USE OF EXTERNAL AIR 18 Version C New closed-circuit wind tunnel (returning leg under ground level) Use of external air optionally Vertical wind tunnel abandoned

CONCLUSIONS ANSWERS 1. All 3 boundary layer wind tunnel types can be realized at the site 2. Open return comes with serious compromises at the specific site 3. Closed circuit tunnel is the ultimative solution however at high costs and with abandonement of the vertical wind tunnel

21 Thank you for your attention!

WIND TUNNEL DESIGN OF ÉTI (1978) 22

inlet Inlet behind screen

24