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NYU/GRUMMAN K-1 AIRFOIL

Cambered · 12% thick · low-to-mid Re
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PROFILENYU/GRUMMAN K-1 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.6% @ 33%c
max camber2.0% @ 74%c
LE radius1.48%c
area upper / chord0.0473
area lower / chord-0.0283
area camber / chord0.0095
TE thickness0.10%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.543-50.3643.3331.27111.672.17820ClAngle 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 0.02281% of chord; maximum error 0.06673%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
142.3
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006905
Maximum Cl
1.951
Angle at maximum Cl (°)
16
Cd at zero lift
0.006913
Cm at zero angle
-0.08664
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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