Similarly shaped airfoils to NACA1412
New! Bulk download of polars in Excel format: NACA1412.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (4) | 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
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2. Ritz 1-30-12
3. HQ 1.0/12
4. NPL 9626
5. MJZ1211
6. AMSOIL2 RUTAN WING
7. NACA63A212
8. NPL 9615
9. NPL 9660
10. ONERA NACA CAMBRE
11. NACA63-212
12. S8038 (13%)
13. NACA64A212
14. NACA63-213
15. NACA64-212
16. NACA63A112
17. NACA63-212 a=0.8
18. NACA63-212 a=0.0
19. NACA64(1)-212
20. NACA63-212 a=0.2
21. NACA64-213