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RAE 5214 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILERAE 5214 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.7% @ 35%c
max camber1.4% @ 69%c
LE radius1.03%c
area upper / chord0.0415
area lower / chord-0.0218
area camber / chord0.0099
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5827-50.32963.3331.24211.672.15420ClAngle 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 0.02467% of chord; maximum error 0.08036%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
143.8
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006437
Maximum Cl
1.926
Angle at maximum Cl (°)
17
Cd at zero lift
0.00644
Cm at zero angle
-0.05585
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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