Similarly shaped airfoils to ZAGI 12
New! Bulk download of polars in Excel format: ZAGI%2012.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
Dynamic plotter New!
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. TsAGI B 11.5% thick
3. NACA M6
4. NACA M6 (NACA-TR-221)
5. NACA 2R212
6. TsAGI B 12.5% thick
7. GOE 677 (= M 6)
8. TsAGI B 11.0% thick
9. EPPLER 361
10. NACA M12 (NACA-TR-221)
11. RAF 34
12. NACA25012
13. EPPLER 360
14. Europa Dykins 12%
15. NACA 2R112
16. GOE 676 (= M 12)
17. NACA24012
18. NACA2212
19. NACA25112
20. RC-12(N)1
21. NACA M12