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AF1600B - Experiment

NACA0012 Aerofoil with Tappings

A 150 mm chord NACA0012 aerofoil with 20 static pressure tappings.

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Description

NACA0012 Aerofoil with Tappings

The aerofoil has 20 static pressure tappings along its chord on the upper and lower surfaces. They each connect to tubes that pass through the aerofoil and then out to clear, numbered, flexible tubes. Students can connect the tubes to other optional pressure-measurement instruments. They can then measure the pressure distribution around the aerofoil, from which they can find the lift.

Using a Pitot tube, students can traverse the aerofoil wake to find the downstream pressure distribution and find the drag on the aerofoil.

Students can compare these values of lift and drag with direct measurements found from a balance. They can also compare them with the results from another aerofoil with the same profile, such as the AF1600d. Varying the angle of attack of the aerofoil with respect to the air stream allows students to find the changes to the pressure distribution. It also allows investigations into the critical conditions at stall.

View the AF1600 experiment flyer here.

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Essential Base Units
Af1600S SUBSONIC WIND TUNNEL 600mm 1118

SUBSONIC WIND TUNNEL 600mm

VDAS AF1600S - Package

TecQuipment’s largest open-circuit subsonic wind tunnel, with a working section of 600 mm by 600 mm and 1250 mm long, is for the study of advanced aerodynamics theory and research. With the larger size comes greater visualisation and more accurate results, operating at meaningful Reynolds numbers.

Alternatives
AF1300 1450 1600h Aircraft Models High Wing 0818

Aircraft Model - High Wing

AF1600H - Experiment

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.

AF1300_1450_1600j 3D Drag Models 0119

Three-Dimensional Drag Models

AF1600J - Experiment

A set of different shape models 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.

AF1300 1450 1600g Aircraft Models Low Wing 0818

Aircraft Model - Low Wing

AF1600G - Experiment

A low wing model aircraft with NACA2415 profile wings for use with TecQuipment's Large Subsonic Wind Tunnel (AF1600S)

AF1300_1450_1600d Two NACA 0012 Aerofoils 1118

Set of Two NACA0012 Aerofoil models

AF1600D - Experiment

This set of two NACA0012 aerofoils allows students to compare the results from a full-width aerofoil with a half width aerofoil.

AF1300_1450_1600c NACA 2414 Aerofoil with Flap 1018

NACA2412 Aerofoil with Variable Flap

AF1600C - Experiment

A 150mm chord NACA2412 aerofoil with 590 span featuring a variable flap that adjusts +/- 90 degrees for use with the AF1600 Subsonic Wind Tunnel.

AF1300_1450_1600a Cylinder Model

CYLINDER MODEL

AF1600A - Experiment

A cylinder model that spans the full width of the working section of the AF1600S Subsonic Wind Tunnel.

Af1600F 1122

Flat Plate Boundary Layer Model Roughened and Smooth

AF1600F - Experiment

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.

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