Similarly shaped airfoils to NACA65A419


New! Bulk download of polars in Excel format: NACA65A419.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. NACA65A420
2. NACA65A418
3. NACA64A419
4. NACA66-419 a=0.8
5. NACA66A419
6. NACA66-519
7. FX 78-PK-188/20
8. NACA65-419 a=0.8
9. NACA65-519
10. NACA64A420
11. NACA66-418 a=0.8
12. NACA65A319
13. NACA66A418
14. NACA65A519
15. NACA66-419 a=0.6
16. NACA66-518
17. NACA65-420 a=0.8
18. NACA65-520
19. GA 40A319
20. GA 37A319
21. NACA66(3)-418