Similarly shaped airfoils to NACA64A314


Direct link: NACA64A314
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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1. NACA63A314
2. NACA65-314 a=0.8
3. GA 37A214
4. NACA65A314
5. NACA65-414
6. GA 35A214
7. NACA65-314 a=0.6
8. GA 40A214
9. NACA65-314
10. GA 40-214
11. NACA64-314 a=0.8
12. NACA65-314 a=0.5
13. LOCKHEED L-188 ROOT
14. GOE 600
15. NACA64-414
16. NACA64A315
17. NACA64A313
18. NACA63A313
19. NACA64-314 a=0.6
20. MS(1)-0313
21. NACA65A313