University of Alberta Facility


 

  • Combustion Wind Tunnel



 

 

The Combustion Wind Tunnel was built in the early 1970’s as one of the features of the Mechanical Engineering Building.  Over the years the tunnel has had many uses including environmental testing, aerodynamic research of low-drag bodies for the Society of Automotive Engineers Super-mileage project, and assisting a ski-jumper in reducing drag during competition. The wind tunnel is a 2 story closed-loop facility.  It has 2 test sections:

      • A large low-speed upper section (2.5m x 2.5m)
      • A smaller high-speed lower section (1.22m x 2.44m).


The tunnel is powered by a 200 HP DC electric motor which can produce constant air speeds up to 36 m/s in the lower test section.  Starting in early 1997, several modifications were made to facilitate the existing tunnel for combustion related research.  These included the following:
 

      • Purge fans to clear combustion products and reactants from the tunnel between tests.
      • A combustible gas detection system and emergency purge control system to prevent dangerous build-ups of explosive gases in the event of a leak.
      • A ceramic roof to prevent the tunnel from burning down.
      • Installation of a window close to the point of combustion so that detailed photographs of the flame could be made.
      • A mobile traverse used for plume characterisation (i.e. current activities: temperature profile of the plume) and single point efficiency measurements.
      • The installation of numerous sensor packages to measure temperatures, wind velocities, gas flow rates, gas concentrations, and more.
  • The Experimental Setup

 

 

To measure the efficiencies of a flare, we ignite the flare in the lower test section of the tunnel and watch the accumulation in concentration of various chemical species within the tunnel. The flares currently burn methane, natural gas, propane, or a combination of these fuels diluted with carbon dioxide and/or nitrogen.  We now put liquid droplets in the gas stream as an additional influencing parameter.

The flare is ignited with a hydrogen flame and the tunnel is brought up to speed in order to test the effects of cross-winds on flare efficiency.  Emissions collect in the tunnel and are measured in real time.  Turbulence generators can be placed upstream of the flare in the tunnel to simulate the gusting and turbulence found in the wind outdoors. 

  • Instrumentation
    • Gas Analyzers


Probably our most important equipment is a suite of 7 online gas analyzers that measure hydrocarbons, carbon dioxide, carbon monoxide, oxygen, oxides of nitrogen, and water vapor.  The following is a list of the components of this system:

- Hydrocarbons – FID (flame ionization detector)
- Carbon Dioxide – NDIR (non-dispersive infrared)
- Carbon Monoxide – NDIR (non-dispersive infrared)
- Oxygen – PMD (paramagnetic detector)
- Nitric Oxide – Chemiluminescent


 

 

 

    • Velocity and Temperature Measurements


The wind tunnel is equipped with various pitot tubes and anemometers in order to measure velocities at different points and at different ranges. Temperature is measured using AD590 constant-current transducers and a variety of thermocouples.
Laser Doppler Velocimetry and hot wire anemometry are used to make very precise measurements of flows and turbulence.  These systems can be mounted on a computer-controlled traverse within the tunnel itself.

    • Flare Stream Measurements


We measure flare gas flows using mass flow controllers.  These devices allow us to measure gas flow rates very accurately.  They are equipped with electronically controlled valves that give us precise control when setting gas flow rates.  Currently, our mass flow meters are calibrated for natural gas, propane, methane, air, carbon dioxide, and nitrogen.  We can adjust the flow meters for other gas types as the need arises.
 

    • Data Acquisition System


Currently, we use a Pentium II 400 MHz computer running National Instruments  LabVIEW software. The computer receives data from all of our various sensor packages through 3 separate data acquistion cards.  As well, the software is used to control the various valves, fans, and pumps throughout the two-story tunnel.  This system allows us to rapidly create or reconfigure our laboratory for varied experiments with a minimum amount of effort.
 

    • Droplet Size Measurement


A laser diffraction size analyser is used to characterize the size distribution of droplets that are added to the gas flare stream.
 

    • Particle Image Velocimeter (PIV)


A PIV is now installed in the Combustion Wind Tunnel. The laser used is a double-pulsed Nd:YAG with a power of 400 mJ/pulse.
  

 

laser and stack
 

During a test. The flame is visible on the left of the picture.

University of Alberta / NRC Facility

 

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Flare Research Project
 

MECHANICAL ENGINEERING DEPARTMENT, UNIVERSITY OF ALBERTA
EDMONTON, ALBERTA, CANADA
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