Similarly shaped airfoils to NACA34013.5


New! Bulk download of polars in Excel format: NACA34013.5.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
Dynamic plotter New!
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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1. NACA34014
2. NACA34013
3. NACA44013.5
4. NACA35013.5
5. NACA44014
6. NACA44013
7. NACA35014
8. EPPLER 625
9. NACA35013
10. NACA25113.5
11. NACA44014.5
12. NACA43013.5
13. NACA25113
14. NACA34014.5
15. NACA35014.5
16. NACA34113
17. EPPLER 327
18. Horten 14.00% thick 4.00% camber
19. Horten 13.00% thick 4.00% camber
20. EPPLER 336
21. EPPLER 342