Similarly shaped airfoils to NACA65-018
New! Bulk download of polars in Excel format: NACA65-018.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (9) | 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. GA 40A018
3. EPPLER 838 HYDROFOIL
4. GA 37A018
5. NACA65-118 a=0.0
6. NACA65-118
7. NACA65-118 a=0.2
8. GA 40-017
9. GA 40A017
10. GA 37-018
11. NACA63A018
12. GA 35A018
13. GA 37A017
14. GA 40-019
15. NACA64-018
16. NACA65-118 a=0.8
17. GA 40A019
18. NACA65-118 a=0.5
19. NACA65-118 a=0.6
20. GA 35A017
21. NACA63A017