Similarly shaped airfoils to NACA35114
New! Bulk download of polars in Excel format: NACA35114.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. NACA35113.5
3. Horten 14.00% thick 5.00% camber
4. Horten 14.00% thick 4.00% camber
5. NACA45114
6. NACA35113
7. NACA45114.5
8. NACA45113.5
9. EPPLER 342
10. NACA44114
11. NACA44113.5
12. NACA44014
13. NACA44114.5
14. Horten 15.00% thick 5.00% camber
15. NACA44013.5
16. Horten 15.00% thick 4.00% camber
17. NACA44014.5
18. Horten 13.00% thick 4.00% camber
19. NACA45115
20. NACA45014
21. NACA45113