BE183-176
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Basic Data: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl | Curve fits | Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Roughness Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Plain Flap Effects: cl,max vs flap deflection: all flap chords | 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cl vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cm vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cd vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
DXF file of spline and points: download
Lednicer-format DAT file download
VisualFoil-format DAT file download
X,Y,Z CSV file download
Selig-format DAT file (download):
Benzing BE 183-176
1.00000000 0.02590000
0.95000000 -0.03840000
0.90000000 -0.08640000
0.80000000 -0.14640000
0.70000000 -0.18650000
0.60000000 -0.21600000
0.50000000 -0.22860000
0.40000000 -0.23190000
0.30000000 -0.22220000
0.20000000 -0.19510000
0.15000000 -0.17260000
0.10000000 -0.14150000
0.07500000 -0.12160000
0.05000000 -0.09730000
0.02500000 -0.06610000
0.01250000 -0.04520000
0.00000000 0.00000000
0.00000000 0.00000000
0.01250000 0.02260000
0.02500000 0.02720000
0.05000000 0.02690000
0.07500000 0.02170000
0.10000000 0.01470000
0.15000000 -0.00070000
0.20000000 -0.01560000
0.30000000 -0.04000000
0.40000000 -0.06010000
0.50000000 -0.07230000
0.60000000 -0.08610000
0.70000000 -0.09160000
0.80000000 -0.09010000
0.90000000 -0.06240000
0.95000000 -0.02790000
1.00000000 0.02690000