Similarly shaped airfoils to NACA64A319


New! Bulk download of polars in Excel format: NACA64A319.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
Dynamic plotter New!
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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1. NACA63A319
2. GA 37A219
3. NACA65-319 a=0.8
4. GA 35A219
5. NACA65-419
6. GA 40A219
7. NACA65-319 a=0.6
8. NACA64A320
9. NACA64A318
10. GA 40-219
11. NACA65-319
12. NACA65A319
13. NACA63A318
14. NACA65-319 a=0.5
15. NACA65-320 a=0.8
16. NACA63A320
17. GA 37A218
18. NACA65-420
19. NACA65A318
20. GA 35A218
21. NACA64A419