Similarly shaped airfoils to NACA4412
New! Bulk download of polars in Excel format: NACA4412.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (350) | 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.
2. CLARK-Y 11.7% smoothed
3. CLARK Y
4. CLARK W
5. GOE 796
6. GOE 693
7. MH139F
8. Davis
9. GOE 623
10. CLARK X
11. NACA4312
12. NM Classic 12 root
13. CLARK K
14. GOE 285
15. GOE 479
16. NACA4413
17. JWL041 11/3.5
18. CLARK Z
19. FX 84-W-127
20. GA 30A412
21. GA 30-412