Similarly shaped airfoils to NACA63A310
New! Bulk download of polars in Excel format: NACA63A310.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. NACA64-310 a=0.8
3. NACA65-310 a=0.8
4. SB98 VS5 tip
5. NACA63-310 a=0.8
6. RAF 28
7. EM CY 1025 20098
8. NACA65A310
9. GA 35A210
10. NACA64-410
11. NACA64-310 a=0.6
12. EM CY 1021 2010 X5 Fertig
13. GA 37A210
14. NACA65-310 a=0.6
15. SG6041
16. NACA65-410
17. TP210-10%
18. NACA65-310
19. NACA64-310
20. EPPLER 224
21. HN-1069c