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AIRCRAFT AND CLASSICCAMBEREDSELIG-DATABASETHIN

D.G.A. 1182

Cambered · 8% thick · low-to-mid Re
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PROFILED.G.A. 1182
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.6% @ 30%c
max camber0.9% @ 40%c
LE radius0.64%c
area upper / chord0.0298
area lower / chord-0.0176
area camber / chord0.0061
TE thickness0.30%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7199-50.12693.3330.973811.671.82120ClAngle 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 0.125% of chord; maximum error 0.5666%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
116.5
Angle at maximum lift / drag (°)
8
Minimum Cd
0.006252
Maximum Cl
1.609
Angle at maximum Cl (°)
15
Cd at zero lift
0.006265
Cm at zero angle
-0.01012
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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