Similarly shaped airfoils to NACA64A313
New! Bulk download of polars in Excel format: NACA64A313.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. NACA65-313 a=0.8
3. NACA65A313
4. GA 37A213
5. NACA65-413
6. NACA65-313 a=0.6
7. GA 35A213
8. NACA65-313
9. GA 40A213
10. NACA64-313 a=0.8
11. GOE 600
12. GA 40-213
13. NACA65-313 a=0.5
14. NACA64-413
15. RAF 31
16. NACA64-313 a=0.6
17. NACA64A314
18. NACA64A312
19. NACA63A312
20. NACA65A312
21. NACA65-314 a=0.8