Similarly shaped airfoils to NACA64A414
New! Bulk download of polars in Excel format: NACA64A414.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. NACA65-414 a=0.8
3. NACA65-514
4. NACA65A414
5. GA 37A314
6. NACA64-414 a=0.8
7. NACA65-414 a=0.6
8. GA 35A314
9. NACA64-514
10. GA 40A314
11. NACA65-414
12. NACA64A415
13. NACA64A413
14. GA 40-314
15. NACA63A413
16. NACA65-415 a=0.8
17. NACA65A413
18. MH 200 12.97%
19. LS(1)-0413 (GA(W)-2)
20. NACA64-415 a=0.8
21. NACA63A415