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AF1300D - Experiment

SET OF 2 NACA 0012 AEROFOIL MODELS

A set of two aerofoils both of NACA0012 profile and 150 mm chord for use with the AF1300 Subsonic Wind Tunnel.

PDF datasheet

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Description

SET OF 2 NACA 0012 AEROFOIL MODELS

A set of two aerofoils. One aerofoil has a span that extends the full width of the working section of the Subsonic Wind Tunnel (AF1300). This model has the characteristics of a two-dimensional aerofoil. The other aerofoil has a span that extends for half of the working section of the wind tunnel. This model has the characteristics of a three-dimensional aerofoil. Comparing the measured lift and drag of the two aerofoils shows the differences between two-dimensional and three-dimensional aerofoils.

Using a Pitot tube, students can traverse the aerofoil wake of the full-width aerofoil. This gives them the downstream pressure distribution to find the drag on the aerofoil. They can compare their results to direct measurements from a balance (available separately).

Students can compare the results from the full-width aerofoil with the tapped aerofoil model (AF1300b, available separately) as it has the same (NACA0012) section.

TecQuipment’s Smoke Generator (AFA11, not included) increases the educational value of the experiments by showing the flow of air around the model.

View the AF1300 experiment flyer here.

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Essential Base Units
SUBSONIC WIND TUNNEL 305 mm Package Af1300S 0618

SUBSONIC WIND TUNNEL 305 mm

VDAS AF1300S - Package

A starter set consisting of the Subsonic Wind Tunnel 305 mm (AF1300), Basic Lift and Drag Balance (AF1300z) and a set of Three-Dimensional Drag Models (AF1300j).

Recommended Ancillaries
Balance Angle Feedback AFA4 1204

BALANCE ANGLE FEEDBACK UNIT

AFA4 - Ancillary

Compact instrument that fixes to the Three Component Balance (AF1300T). It measures the angle positions of models mounted in the balance and feeds the information directly to the Versatile Data Acquisition System (VDAS®).

Differential pressure transducer AFA5 0804

DIFFERENTIAL PRESSURE TRANSDUCER

AFA5 - Ancillary

Digital differential pressure measurement and display unit for use with TecQuipment’s Subsonic Wind Tunnel (AF1300).

Afa7 Pitot Static Traverse

PITOT STATIC TRAVERSE (DIGITAL)

AFA7 - Ancillary

A traversing Pitot static tube with electronic position measurement for use with TecQuipment’s Subsonic Wind Tunnels (AF1300, AF1300s, AF1600s).

THREE COMPONENT BALANCE Af1300T

THREE COMPONENT BALANCE

AF1300T - Ancillary

Supports wind tunnel models in the AF1300 Subsonic Tunnel and measures their lift, drag and pitching moment.

BASIC LIFT AND DRAG BALANCE AF1300z 0619

BASIC LIFT AND DRAG BALANCE

AF1300Z - Ancillary

A two-component balance that measures lift and drag forces on models mounted in the AF1300 Subsonic Wind Tunnel.

Alternatives
Drag Force Af12 0404

DRAG FORCE

AF12 - Experiment

Allows students to investigate the direct and indirect measurement of drag on various shapes and to calculate and analyse the drag coefficient by different methods.

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