Similarly shaped airfoils to NACA35112
New! Bulk download of polars in Excel format: NACA35112.xlsx
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
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2. HS 3.5/12
3. Horten 12.00% thick 5.00% camber
4. NACA35113
5. HS 3.4.12b
6. NACA44112
7. EPPLER 637
8. M-35A-12.7
9. NACA44012
10. NACA34112
11. Horten 13.00% thick 4.00% camber
12. Horten 13.00% thick 5.00% camber
13. EPPLER 636
14. Horten 11.00% thick 4.00% camber
15. NACA45113
16. NACA45012
17. NACA35012
18. Horten 11.00% thick 5.00% camber
19. EPPLER 332
20. NACA45112
21. NACA35113.5