Similarly shaped airfoils to NACA6212


New! Bulk download of polars in Excel format: NACA6212.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (6) | 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. GOE 321 (HANSA-BRANDENBURG III.1)
2. GOE 365
3. SPICA 11.73% smoothed
4. GOE 509
5. GOE 530
6. USA 27
7. EPPLER 639
8. GOE 406
9. GOE 404
10. NACA M21 (NACA-TR-221)
11. NACA M21
12. GOE 324 (HANSA-BRANDENBURG)
13. GOE 584
14. GOE 591
15. GOE 323 (HANSA-BRANDENBURG V.1)
16. NACA M9 (NACA-TR-221)
17. GOE 319 (HANSA-BRANDENBURG II)
18. GOE 418
19. GOE 532
20. St. CYR 24 (Bartel 35-IIIC)
21. GOE 322 (HANSA-BRANDENBURG IV.1)