Similarly shaped airfoils to NACA 6-H-20
New! Bulk download of polars in Excel format: n6h20.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
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. NACA65-720 a=0.2
3. NACA66-720 a=0.2
4. NACA66-719 a=0.2
5. NACA65-720 a=0.5
6. NACA66-720 a=0.5
7. GOE 424
8. NACA66-719 a=0.5
9. NACA65-719 a=0.2
10. GOE 383
11. GA 40A620
12. GA 40-620
13. GA 37A620
14. NACA65-719 a=0.5
15. NACA66-718 a=0.2
16. DRAGONFLY CANARD
17. FX 08-S-176
18. GA 35A620
19. NACA66-718 a=0.5
20. GA 37A619
21. GA 40A619