Similarly shaped airfoils to NACA23112
New! Bulk download of polars in Excel format: NACA23112.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. NACA32012
3. NACA32112
4. NACA22112
5. NACA22012
6. NACA24112
7. NACA23113
8. Horten 12.00% thick 2.00% camber
9. NACA23013
10. NACA32013
11. Horten 12.00% thick 1.00% camber
12. MJZ1211
13. NACA32113
14. GOE 766
15. NACA24113
16. MH 106 13.07%
17. NACA22113
18. NACA22013
19. ONERA NACA CAMBRE
20. NACA42012
21. Horten 13.00% thick 2.00% camber