Similarly shaped airfoils to NACA63A418
New! Bulk download of polars in Excel format: NACA63A418.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (7) | 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. GA 35A318
3. NACA65-418 a=0.8
4. NACA63A419
5. NACA63A417
6. GA 37A318
7. NACA65-518
8. NACA64A419
9. NACA64-418 a=0.8
10. NACA64-518
11. NACA64-419 a=0.8
12. NACA64-519
13. NACA64A417
14. LS(1)-0417 (GA(W)-1)
15. NACA65-418 a=0.6
16. NACA64(3)-418
17. NACA63A318
18. NACA65-419 a=0.8
19. NACA63A518
20. NACA64-418 a=0.6
21. NACA65-418