Similarly shaped airfoils to NACA64(1)-212 MOD A


New! Bulk download of polars in Excel format: n64212ma.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. DEFIANT CANARD BL145
2. NM32 root
3. LDS-2
4. GA 30-312
5. NACA63-512 a=0.0
6. EPPLER 207
7. HQ 2.5/12
8. NACA64-512 a=0.0
9. GA 35-312
10. GA 37-312
11. NACA63-412 a=0.2
12. SIKORSKY SC1012R8
13. GA 35A312
14. FX 68-H-120
15. MS2.5/13GPV
16. GA 35-313
17. NACA64-412 a=0.2
18. HQ 2.0/12
19. NACA63-513 a=0.0
20. FAD24
21. GA 37-313