Similarly shaped airfoils to NACA63A313
New! Bulk download of polars in Excel format: NACA63A313.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. GA 35A213
3. GOE 600
4. NACA65-313 a=0.8
5. NACA64-313 a=0.8
6. GA 37A213
7. RAF 31
8. NACA64-413
9. NACA64-313 a=0.6
10. NACA65-313 a=0.6
11. NACA65-413
12. NACA63-313 a=0.8
13. NACA64-314 a=0.8
14. NACA65-313
15. GA 40A213
16. NACA65A313
17. NACA64-313
18. GA 40-213
19. NACA64-414
20. NACA63A314
21. NACA63A312