Research Facilities

Fluids Laboratory

Major equipment:

  • Wave tank: 52m long c/w towing carriage capable of 5.0m/s maximum speed
  • Wind tunnel: 4' height x 3' width c/w aero lab 6 axis dynamometer
  • Deep water tank: 12' x 12' x 13' max water depth with access to 1t overhead crane
  • Open water flume: 32' long x 17" wide x 22" deep
  • Portable flume: 7' long x 6" wide x 12" deep
  • Riverbed Flume: 16' long x 16" wide x 8" deep with a sand bottom
  • Multi phase flow loop: petroleum reservoir simulator
  • Open boat used for open water propeller testing
  • Trim tank: 12' x 3' x 1'- 8" deep

Materials Characterization Research Laboratory

  • X-ray Diffraction (XRD)-(Rigaku D/MAX 2200VPC)
  • Scanning Electron Microscope (SEM)-(Cambridge Stereoscan 200 SEM)
  • Chemical Analysis Detector on SEM performs Energy Dispersive Spectroscopy (EDS)-(Oxford Link 6139 EDS)
  • Digital Imaging on SEM and Optical Microscopes by Image Analysis System (IAS)-(Image Analysis Software with Digital Storage)
  • Metallograph-(Reichert)
  • Various Optical Microscopes and Cameras-(Zeitz Metallovert, Wild Makroskop M420, Olympus, adaptors for Digital Imaging)
  • Darkroom Film Processing

Corrosion Research Laboratory

  • Potentiostat/Galvanostat-(Princeton Applied Research Company-PARC 283)
  • Electrochemical Probes and Data Aquisition Software (Labview)

Metallurgy and Tribology Research Laboratory

  • Heat Treatment
  • Mechanical Testing
  • Non-Destructive Testing (NDT)
  • Metallography Research Equipment and Laboratories

Heat Treatment Research Laboratory

  • Furnaces for Melting
  • Casting and Annealing Heat Treatments-(Tube and Pot Furnaces-Lindberg; Box Furnace-Thermolyne; and High Temperature Furnace-Burrell)

Mechanical Testing Research Laboratory

  • Tension and Compression Testers-(Instron , Instron 1123, Instron 8874 (10,000N axial 100N-m rotational), MTS 312.21 (200,000N axial 80N-m rotational), MTS-Instron 8801 and MTS 312.21 System
  • Impact Tester-(Avery)
  • Rockwell Harness Tester-(Wilson)
  • Micro-hardness Tester-(Micromet)
  • Hydaulic Press-(Vega)
  • Motion Analysis-(Peak Six Camera Real-Time and VCR)

Non-destructive Testing (NDT) Research Laboratory

  • Liquid Dye Penetrant-Fluorescent-UV Light and Magnetic Particle Inspection-Magnaflux MagII

Metallography Research Laboratory

  • Cutting-Metaserv Cut-Off Machine
  • Hot and Cold Metal Sample Preparation Equipment
  • Hydraulic Press-(Vega)
  • Grinding-(Buhler Surfmet)
  • Polishing-(Struers Polishing Table, Various Buehler Metaserv Minimet, Isomet Polishers and Electropolisher)
  • Chemical Etching and Ultrasonic Cleaning
  • Weigh Balances-(Mettler)

Thermal Fluids Laboratory

The thermal and fluids laboratories within the mechanical engineering department contain a number of facilities for conducting experimental studies in fluid dynamics and heat transfer. In addition to those listed below, the ocean and naval engineering department also maintains a 58 m tow tank with wave generation capabilities and a deep water test tank. The civil department also maintains a water flume of approximately 2' cross-section. Facilities for conducting research in electronics cooling, process flow and heat transfer, and heat exchanger modeling include:

  • 36" Low Speed Wind Tunnel: Open circuit wind tunnel with a 3' x 3' test section. Airflow is controlled using a vane damper at the fan inlet. Air speed can be varied from 0-15 m/s (0 – 30000 CFM). Data acquisition is fully automated using a PC/Data logging system using Labview.
  • 12" Low Speed Variable Orientation Wind Tunnel: This unique, multi-purpose wind tunnel is designed for mixed and forced convection testing for horizontal, vertical and inclined geometries. By rotating the test section and duct assembly about a pivot axis coincident with the centre line of the blower, the test section can be set to any angle between vertical and horizontal. The contraction section in the inlet plenum has a 9:1 contraction ratio and a 10 cm (4 in.) thick honeycomb flow straightener that reduces non-uniformities in the mean flow field and produces a relatively uniform velocity profile at the entrance of the test section. The removable, 30 cm x 30 cm x 60 cm (12" x 12" x 24") test section is generally large enough to accomodate most common test specimens. Airflow velocities of 0 - 15 m/s (0 - 3000 CFM) are controlled using a TB Woods frequency-based speed regulator.
  • 6” Low Speed Multi-Purpose Wind Tunnel and Impingement Flow Facility: These two wind tunnels were designed for examining thermal performance of heat sinks and other air cooled assemblies such as automotive radiators. The flexible modular design allows for custom test sections to accommodate a number of applications including impingement flow in electronics cooling and air cooled automotive radiators. The tunnel is equipped with a 500 CFM variable speed fan. Maximum air velocity at open section is approximately 10 m/s. A companion facility allows for vertical jet impingement cooling studies to be performed.
  • 3” Multi-Phase/Two Phase Flow Loop: A 3" diameter two phase flow loop has been constructed at Memorial to investigate oil-water-gas flows. The facility was initially designed to support the development of an electro-quasi-static multi-phase flow meter (MPFM) to measure the individual oil-water-gas flow rates of unprocessed oil well streams. The flow loop is a 65 m re-circulating open circuit system, and is constructed of 3-inch diameter pipe. There are clear horizontal and vertical test sections for flow visualization and measurements. Instrumentation includes several pressure and temperature transducers, and flow meters on the gas and liquid lines to measure the individual gas and liquid flow rates. Electro-pneumatic control valves are installed on the liquid and air lines to facilitate control of the flow conditions, and a wide range of flow regimes can be generated. Operational control of the loop is implemented through a fully integrated computer system which is also used for data acquisition and high speed imaging. Quantitative flow visualization techniques, in combination with hot-film anemometry measurements have been used to study and characterize the different flow regimes. The system is also equipped with a laser based Particle Image Velocimetry (PIV) system to aid in velocity and flow composition analysis and a variable speed pump controller.
  • Mini Single and Two Phase Flow Loop: This new flow loop was designed to study single and two phase flow characteristics in minichannels and compact heat exchanger cores. It allows both the thermal and hydraulic characteristics of compact heat exchanger cores and liquid cooled electronics assemblies to be determined. Typical flow range would allow liquid flows to vary from 0.05 – 60 Lpm of liquid flow using a variable speed pump, 0 – 50 Lpm of air flow provided by a compressor, pressure measurement in the range of 0 - 60 psig, and fluid operating temperatures up to 120 C. Various test fluids will be used such as glycerin, glycol, automotive oils, water, and water/glycol mixtures. The facility also allows for liquid to liquid, liquid to air cooling, and liquid cooling only, studies to be conducted. Thermal input is provided through a constant temperature fluid reservoir or by means of electric heaters using a 1200 W power supply. Data acquisition is fully automated using Labview.


Mechanical Engineering

230 Elizabeth Ave

St. John's, NL A1B 3X9 CANADA

Tel: (709) 864-2530

Fax: (709) 864-2552