A pair of boundary layer models with a mounting plate, also a pitot and a static probe for investigating boundary layer. One plate is roughened, the other smooth to allow comparisons on boundary layer growth.
The Pitot and static tubes fit to the Pitot-static XY traverse to allow pressures to be measured very close to the flat plate’s surface. The traverse allows the boundary layer to be measured at multiple positions.
This is an ancillary for the AF1600 Subsonic Wind Tunnel.
AF1600S - Package
An open circuit suction subsonic wind tunnel with a working section of 600 mm by 600 mm and 1250 mm long. Package includes a Three-Component Balance, Dual Axis Pressure Traverse and associated instrumentation such as a 32-Way Pressure Display Unit and Versatile Data Acquisition System (VDAS-F).
The high wing model aircraft with NACA profile wings for use with the Large Subsonic Wind Tunnel (AF1600) is good for experiments with lift, drag and pitching moment of fixed wing aircraft.
A low wing model aircraft with NACA2415 profile wings for use with TecQuipment's Large Subsonic Wind Tunnel (AF1600S)
A set of different shape models for use with the Large Subsonic Wind Tunnel (AF1600S) each with identical frontal area to allow students to compare the different coefficient of drag for each shape. Includes a dummy stem for tests to cancel out the drag due to each model’s support arm.
This set of two NACA0012 aerofoils allows students to compare the results from a full-width aerofoil with a half width aerofoil.
A 150mm chord NACA2412 aerofoil with 590 span featuring a variable flap that adjusts +/- 90 degrees for use with the AF1600 Subsonic Wind Tunnel.
A 150 mm chord NACA0012 aerofoil with 595 mm span and 20 static pressure tappings.
A cylinder model that spans the full width of the working section of the AF1600S Subsonic Wind Tunnel.