Similarly shaped airfoils to NACA34113.5
New! Bulk download of polars in Excel format: NACA34113.5.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. NACA34114.5
3. NACA43013.5
4. EPPLER 341
5. NACA34113
6. EPPLER 625
7. Horten 14.00% thick 3.00% camber
8. EPPLER 340
9. NACA33113.5
10. Horten 13.00% thick 3.00% camber
11. Horten 14.00% thick 4.00% camber
12. EPPLER 336
13. NACA44113.5
14. NACA33113
15. NACA25113.5
16. NACA44114
17. Horten 13.00% thick 4.00% camber
18. NACA33114
19. NACA44013.5
20. NACA44014
21. NACA44113