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AF1300E - Experiment

100 MM DIAMETER FLAT PLATE

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

PDF datasheet

OR CALL US TO DISCUSS +44 1159 722 611

Description

100 MM DIAMETER FLAT PLATE

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 AF1300 wind tunnel) supports the model in the tunnel. Alternatively, either the optional Three-Component Balance (AF1300t, available separately) or the Single-Component Lift and Drag Balance (AF1300z, available separately) can hold the model and measure the drag.

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
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.

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).

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.

Flutter Wing 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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