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AF1300E - Experiment

FLAT PLATE DRAG MODEL

A 100 mm diameter flat plate for use with the AF1300 Subsonic Wind Tunnel.

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Description

FLAT PLATE DRAG MODEL

This model shows the flow around a bluff body mounted normal to the air flow direction, and the drag force exerted on it.
A holder (included with the AF100 wind tunnel) supports the model in the tunnel. Alternatively, either the optional Three-Component Balance (AFA3, available separately) or the Single-Component Lift and Drag Balance (AFA2, available separately) can hold the model and measure the drag.
TecQuipment’s Smoke Generator (AFA10, not included) increases the educational value of the experiments by showing the flow of air around the model.

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Essential Base Units
Af1300S 0618

SUBSONIC WIND TUNNEL 305 mm

VDAS AF1300S - Package

An open circuit suction subsonic wind tunnel with a working section of 300 mm by 300 mm and 600 mm long.

Recommended Ancillaries
Af1300T

THREE COMPONENT BALANCE

AF1300T - Ancillary

A three-component balance designed for use with the AF1300 Subsonic Wind Tunnel.

AFA5

DIFFERENTIAL PRESSURE UNIT

AFA5 - Ancillary

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

Afa7 0118 Small Copy

PITOT STATIC TRAVERSE (DIGITAL)

AFA7 - Ancillary

A traversing Pitot-static tube with electronic position measurement for use with TecQuipment’s Subsonic Wind Tunnels (AF1300, AF1450, AF1600).

AF1300z 0619

BASIC LIFT AND DRAG BALANCE

AF1300Z - Ancillary

A two-component balance to measure the lift and drag forces on models mounted in an AF1300 Subsonic Wind Tunnel.

Alternatives
Drag Force Af12 0404

DRAG FORCE

AF12 - Experiment

An experimental module for use with the AF10 Air Flow Bench to provide experiments that measure and compare the effects of drag force on objects mounted in an airstream that have the same projected frontal area but different shape. Facilities to compare drag force measurement methods are included.

Af1300R 0920

Flutter Wing

VDAS AF1300R - Experiment

An aerofoil suspended on springs within a frame, used to demonstrate wing flutter. The suspension positions of the wing can be altered, as can the angle of attack.

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