Similarly shaped airfoils to NACA34117
New! Bulk download of polars in Excel format: NACA34117.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
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2. NACA44117
3. Horten 17.00% thick 4.00% camber
4. NACA44116.5
5. NACA34118
6. NACA34116
7. NACA34017
8. Horten 17.00% thick 3.00% camber
9. Horten 18.00% thick 4.00% camber
10. NACA35117
11. NACA34016.5
12. NACA33117
13. NACA44118
14. NACA33116.5
15. NACA35116.5
16. NACA44017
17. Horten 18.00% thick 3.00% camber
18. NACA34018
19. NACA35118
20. NACA25117
21. NACA34016