Similarly shaped airfoils to NACA65A318
New! Bulk download of polars in Excel format: NACA65A318.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. NACA66-318 a=0.8
3. NACA66A318
4. NACA65A319
5. NACA65A317
6. NACA66-418
7. NACA66-318 a=0.6
8. GA 40A218
9. GA 37A218
10. NACA65-318 a=0.8
11. NACA65-418
12. NACA64A319
13. NACA66-317 a=0.8
14. NACA66A317
15. GA 40-218
16. NACA65-319 a=0.8
17. NACA66-318
18. NACA66-318 a=0.5
19. NACA65-318 a=0.6
20. NACA65-419
21. GA 40A219