Airfoils.Pro
database / Research / RAE 5213
CAMBEREDRESEARCHSELIG-DATABASE

RAE 5213

Cambered · 10% thick · low-to-mid Re
Compare↓ Download
PROFILERAE 5213
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.9% @ 35%c
max camber1.4% @ 69%c
LE radius1.09%c
area upper / chord0.0426
area lower / chord-0.0218
area camber / chord0.0104
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5782-50.33293.3331.24411.672.15520ClAngle 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 0.02445% of chord; maximum error 0.0762%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
144
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006459
Maximum Cl
1.927
Angle at maximum Cl (°)
17
Cd at zero lift
0.006464
Cm at zero angle
-0.05635
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…