Similarly shaped airfoils to NACA63-510 a=0.5
New! Bulk download of polars in Excel format: NACA63-510%20a%3D0.5.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. NACA63-510 a=0.6
3. GA 35-410
4. GA 37-410
5. NACA64-510 a=0.6
6. EPPLER 193
7. GA 35A410
8. S3024 9.84%
9. EPPLER E193gU-K24
10. NACA65-510 a=0.5
11. GA 37A410
12. GA 40-410
13. GA 40A410
14. S4061-096-84
15. SD6080 (9.2%)
16. S3025 9.38%
17. GA 30-410
18. NACA65-510 a=0.6
19. NACA63-511 a=0.5
20. NACA63-509 a=0.5
21. GA 35-411