Experiment
AF1300L
S1210 AEROFOIL
An S1210 profile aerofoil of 60mm chord for use with the AF1300 Subsonic Wind Tunnel.
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+44 1159 722 611S1210 AEROFOIL
An unsymmetrical aerofoil that spans the full width of the working section of the Subsonic Wind Tunnel (AF1300), for two-dimensional experiments. This aerofoil has an S1210 profile, based on a design originated by Michael S Selig of the University of Illinois. It provides excellent lift at low Reynolds numbers for high-lift, low-speed applications.
Ancillary
AFA5
DIFFERENTIAL PRESSURE TRANSDUCER
Ancillary
AFA7
PITOT STATIC TRAVERSE (DIGITAL)
Ancillary
AF1300Z
BASIC LIFT AND DRAG BALANCE
Experiment
AF12
DRAG FORCE
Experiment
AF1300R