Similarly shaped airfoils to AMSOIL1 RUTAN CANARD


New! Bulk download of polars in Excel format: amsoil1.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. S8055 (12%)
2. CB2012
3. NACA M12
4. GOE 676 (= M 12)
5. LDS-2
6. NACA64A312
7. NACA63A312
8. GA 37A212
9. GA 35A212
10. NACA65-312 a=0.6
11. NACA65-312 a=0.5
12. NACA M12 (NACA-TR-221)
13. EM CY 1016 2012
14. GA 30A212
15. NACA65A312
16. GA 30-212
17. GOE 548
18. Ritz 2-30-12
19. NACA65-312 a=0.8
20. NACA65-412
21. GA 40A212