Similarly shaped airfoils to NACA63-410 a=0.5
New! Bulk download of polars in Excel format: NACA63-410%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. NACA63-410 a=0.6
3. FX 84-W-097
4. NACA64-410 a=0.6
5. GA 35-310
6. GA 37-310
7. EPPLER EB380
8. GA 35A310
9. S3014-095-85
10. NACA65-410 a=0.5
11. S3021-095-84
12. GA 37A310
13. GA 40-310
14. GA 40A310
15. NACA65-410 a=0.6
16. MH 117 9.8%
17. NACA63-510 a=0.0
18. SD2083 (9.0%)
19. NACA63-410 a=0.8
20. NACA64-510 a=0.0
21. GA 30-310