Airfoils.Pro
database / Other families / WHITCOMB INTEGRAL SUPERCRITICAL
CAMBEREDOTHER FAMILIESSELIG-DATABASE

WHITCOMB INTEGRAL SUPERCRITICAL

Cambered · 11% thick · low-to-mid Re
Compare↓ Download
PROFILEWHITCOMB INTEGRAL SUPERCRITICAL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.0% @ 35%c
max camber2.3% @ 82%c
LE radius1.32%c
area upper / chord0.0435
area lower / chord-0.0300
area camber / chord0.0068
TE thickness0.05%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3946-50.51393.3331.42211.672.33120ClAngle 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 0.04209% of chord; maximum error 0.1913%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
150.7
Angle at maximum lift / drag (°)
9
Minimum Cd
0.007134
Maximum Cl
2.104
Angle at maximum Cl (°)
16
Cd at zero lift
0.007195
Cm at zero angle
-0.1314
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…