Similarly shaped airfoils to NACA65-419 a=0.8
New! Bulk download of polars in Excel format: NACA65-419%20a%3D0.8.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. NACA65-419 a=0.6
3. NACA64A419
4. GA 40-319
5. GA 40A319
6. NACA65-419
7. NACA65-419 a=0.5
8. NACA65-420 a=0.8
9. NACA65-418 a=0.8
10. NACA65-520
11. NACA63A419
12. NACA65-518
13. NACA64A418
14. NACA65(421)-420
15. NACA64-419 a=0.8
16. NACA64-519
17. NACA65-418 a=0.6
18. NACA65-420 a=0.6
19. GA 37A319
20. NACA65A419
21. NACA65-619