Similarly shaped airfoils to NACA63A309
New! Bulk download of polars in Excel format: NACA63A309.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. NACA64-309 a=0.8
3. NACA65-309 a=0.8
4. NACA63-309 a=0.8
5. NACA65A309
6. S2048
7. HS 1.7/9
8. NACA64-309 a=0.6
9. NACA64-409
10. RG-15 8.9%
11. NACA65-309 a=0.6
12. NACA65-409
13. HN-350M01
14. TP202-9%
15. HQ-2.0/9 9.0% smoothed
16. HN-184
17. DP1.72/8.32_DS
18. HQ 2.0/9
19. NACA2409
20. NACA63-409
21. NACA65-309