Similarly shaped airfoils to NACA45117
New! Bulk download of polars in Excel format: NACA45117.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 5.00% camber
3. Horten 17.00% thick 6.00% camber
4. NACA45118
5. NACA45116
6. Horten 18.00% thick 5.00% camber
7. Horten 16.00% thick 5.00% camber
8. Horten 18.00% thick 6.00% camber
9. NACA35117
10. NACA35116.5
11. Horten 16.00% thick 6.00% camber
12. NACA44116
13. NACA45017
14. NACA35116
15. NACA45016.5
16. Horten 16.00% thick 4.00% camber
17. NACA35118
18. NACA45018
19. NACA45016
20. NACA45115
21. NACA44017