Similarly shaped airfoils to NACA2309
New! Bulk download of polars in Excel format: NACA2309.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (3) | 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. RG 14 9%
3. MH 42 8.94%
4. RG 14
5. S6061 9%
6. NACA2409
7. HS 1.7/9
8. DD928416
9. TP202-9%
10. JWL075 8.8/1.76
11. RG-12A 9.00%
12. RG 12A-1.8/9.0
13. FAD13
14. TL55
15. HN-163TA
16. NACA25009
17. RG 14 9.5%
18. RG-15 8.9%
19. Ritz 2-30-10
20. HQ 1.5/9
21. HN-1054