Similarly shaped airfoils to NACA65A319
New! Bulk download of polars in Excel format: NACA65A319.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. NACA65A318
3. NACA64A319
4. NACA66-319 a=0.8
5. NACA66A319
6. NACA66-419
7. GA 40A219
8. GA 37A219
9. NACA66-319 a=0.6
10. NACA65-319 a=0.8
11. NACA64A320
12. NACA65-419
13. NACA66-318 a=0.8
14. NACA65A419
15. NACA66A318
16. GA 40-219
17. NACA65A219
18. GA 40A220
19. NACA65-320 a=0.8
20. NACA66-418
21. NACA65-420