Similarly shaped airfoils to NACA45112
New! Bulk download of polars in Excel format: NACA45112.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
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. Horten 12.00% thick 6.00% camber
3. Horten 13.00% thick 5.00% camber
4. Horten 11.00% thick 5.00% camber
5. Horten 13.00% thick 6.00% camber
6. NACA45113
7. NACA35112
8. NACA45110.5
9. Horten 11.00% thick 6.00% camber
10. EPPLER 638
11. NACA45012
12. NACA45113.5
13. RAF 33
14. NACA35113
15. EPPLER 334
16. NACA45013
17. HS 3.5/12
18. EPPLER 637
19. NACA45110
20. NACA44012
21. NACA44110.5