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CAMBEREDRESEARCHSELIG-DATABASE

RAF 34 AIRFOIL

Cambered · 13% thick · low-to-mid Re
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PROFILERAF 34 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.6% @ 30%c
max camber2.0% @ 30%c
LE radius1.76%c
area upper / chord0.0523
area lower / chord-0.0317
area camber / chord0.0103
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6737-50.15593.3330.985511.671.81520ClAngle of attack (°)
Why this curve

This is a NeuralFoil prediction from the stored profile coordinates and the selected flow condition, with AeroSandbox compressibility corrections. It is not a completed OpenFOAM calculation.

Prediction error has not been calibrated for this condition. No accuracy interval is claimed.

Geometry fit: RMS error 0.05596% of chord; maximum error 0.2746%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
118.6
Angle at maximum lift / drag (°)
11
Minimum Cd
0.007156
Maximum Cl
1.608
Angle at maximum Cl (°)
16
Cd at zero lift
0.007183
Cm at zero angle
-0.00315
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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