Similarly shaped airfoils to NACA63A409
New! Bulk download of polars in Excel format: NACA63A409.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. NACA64-409 a=0.8
3. NACA65-409 a=0.8
4. NACA63-409 a=0.8
5. NACA64-509
6. NACA65-509
7. NACA65A409
8. NACA63-509
9. HQ 2.5/9
10. HN-227
11. HN-350M02
12. HN-380
13. HN-839D
14. HQ 2.5/9.0 smoothed by Eppler
15. HQ 2.5/9 B
16. HN-184M
17. SD2030-086-88
18. NACA64-409 a=0.6
19. WSM825
20. NACA65-409 a=0.6
21. NACA64-410 a=0.8