Similarly shaped airfoils to NACA65-418
New! Bulk download of polars in Excel format: NACA65-418.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (10) | 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. NACA65-318 a=0.6
3. GA 40-218
4. GA 40A218
5. NACA64A318
6. NACA65-318 a=0.5
7. NACA65-418 a=0.8
8. NACA65-419
9. NACA65-417
10. NACA65-318
11. NACA65-317 a=0.8
12. NACA65-518
13. EPPLER 544
14. GA 37A218
15. NACA63A318
16. NACA65-319 a=0.8
17. NACA64-418
18. NACA64A418
19. EPPLER 545
20. NACA64A317
21. NACA65-317 a=0.6