Similarly shaped airfoils to NACA35117
New! Bulk download of polars in Excel format: NACA35117.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. Horten 17.00% thick 4.00% camber
3. NACA35118
4. NACA35116
5. Horten 17.00% thick 5.00% camber
6. NACA44017
7. NACA34117
8. NACA44117
9. NACA44116.5
10. NACA34116.5
11. Horten 16.00% thick 4.00% camber
12. NACA44016.5
13. Horten 18.00% thick 4.00% camber
14. Horten 18.00% thick 5.00% camber
15. NACA45017
16. NACA44116
17. NACA34116
18. NACA44018
19. NACA45016.5
20. NACA45117
21. Horten 16.00% thick 5.00% camber