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CAMBEREDRESEARCHSELIG-DATABASE

OAF095 AIRFOIL

Cambered · 9% thick · low-to-mid Re
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PROFILEOAF095 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.5% @ 24%c
max camber3.8% @ 53%c
LE radius0.99%c
area upper / chord0.0526
area lower / chord-0.0053
area camber / chord0.0237
TE thickness0.52%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2781-50.5873.3331.45211.672.31720ClAngle 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 0.005246% of chord; maximum error 0.02437%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
145.6
Angle at maximum lift / drag (°)
9
Minimum Cd
0.007117
Maximum Cl
2.101
Angle at maximum Cl (°)
16
Cd at zero lift
0.007119
Cm at zero angle
-0.1319
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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