Similarly shaped airfoils to NACA34015


New! Bulk download of polars in Excel format: NACA34015.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. Horten 15.00% thick 3.00% camber
2. NACA33015
3. NACA25115
4. NACA34016
5. NACA33014.5
6. NACA25114.5
7. NACA25015
8. NACA34115
9. NACA34114.5
10. NACA25014.5
11. Horten 16.00% thick 3.00% camber
12. NACA44015
13. NACA33115
14. NACA33014
15. NACA34014.5
16. Horten 14.00% thick 3.00% camber
17. NACA33114.5
18. Horten 15.00% thick 2.00% camber
19. NACA25114
20. NACA44014.5
21. SSV2316 VANS RV-10