Room(s): EAS 3330
Area: 920 sq. ft.
Mission:
To expose the student to experiments related
to the mechanics of fluids, internal viscous
flow, and flow around immersed bodies.
Equipment:
The lab has nine principal pieces of teaching
equipment that are used in performing a variety
of experimental exercises.
Fluid flow experiments
Jet Impact (Conservation of Linear Momentum).
Orifice Flow (includes orifice accessory set).
Venturi Meter (Application of Bernoulli’s Equation).
Reynolds Transition (Flow Visualization).
Laminar and Turbulent Pipe Friction (Darcy Friction Factor).
Minor Pipe-work Losses.
Free-standing experiments
Flow Visualization Water Tunnel (6” test
section): An un-pressurized, closed circuit
flow loop with a three color dye injection
system. Available
flow models include airfoils, cylinders (cross flow), spheres, ellipsoids,
cones, and hemispherical cups. Additionally, weir and sluice gates can be configured.
Subsonic Wind Tunnel (12” test section): Closed-flow loop device with
electronic pressure transducers, probe traversing mechanism, and a two-axis
force balance (dynamometer). Flow models include NACA 0012 and 4412 airfoils
with pressure taps, cross-flow cylinders with pressure taps, various blunt
bodies for drag force experiments.
Blower/Duct Apparatus: Centrifugal blower attached to an instrumented 8” duct.
Various reducers, elbows, and exhaust pieces can be fitted. Experiments involving
air speed measurement, velocity profiles in ducts, minor losses, etc. can be
conducted with this system.
All of the above equipment except for the
wind tunnel and the blower/duct apparatus,
was purchased in the last four years (capital
improvement of $26,350).
Students: The laboratory can accommodate
twelve students simultaneously operating
four experimental stations. |