Similarly shaped airfoils to NACA65-519
New! Bulk download of polars in Excel format: NACA65-519.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. NACA65-520
7. NACA65-518
8. NACA65-418 a=0.8
9. NACA65(421)-420
10. NACA65-419
11. NACA65-420 a=0.8
12. NACA65-619
13. NACA63A419
14. NACA65-419 a=0.5
15. NACA64A418
16. NACA64-519
17. GA 37A319
18. NACA65-519 a=0.8
19. NACA65A419
20. NACA65A418
21. FX 05-188