Similarly shaped airfoils to NACA 2R112


New! Bulk download of polars in Excel format: NACA2R112.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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1. NACA2212
2. GA 30A212
3. NACA2312
4. NACA M12 (NACA-TR-221)
5. GA 30-212
6. GOE 676 (= M 12)
7. NACA M12
8. NACA25012
9. Ritz 2-30-12
10. GOE 677 (= M 6)
11. RAF 34
12. NACA2412
13. NACA 2R212
14. S8055 (12%)
15. ONERA OA212
16. NACA M6
17. NACA M6 (NACA-TR-221)
18. S8052 (11.88%)
19. ZAGI 12
20. TsAGI B 12.0% thick
21. CB2012