Similarly shaped airfoils to NACA25017
New! Bulk download of polars in Excel format: NACA25017.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (5) | 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. NACA25016.5
3. Horten 17.00% thick 2.00% camber
4. NACA24016.5
5. NACA25117
6. NACA24117
7. NACA24116.5
8. NACA23017
9. NACA25116.5
10. NACA25018
11. NACA25016
12. NACA33017
13. NACA24016
14. NACA23016.5
15. NACA2218
16. NACA23017.424
17. Horten 18.00% thick 2.00% camber
18. NACA24018
19. NACA33016.5
20. NACA23117
21. Horten 16.00% thick 2.00% camber