Similarly shaped airfoils to NACA 8-H-12
New! Bulk download of polars in Excel format: n8h12.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (24) | 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. NACA63-612 a=0.0
3. NACA63-512 a=0.2
4. HS 3.4.12b
5. NACA63-512 a=0.0
6. NACA64-612 a=0.0
7. AH 80-136
8. NACA64-512 a=0.2
9. HS 3.5/12
10. BOEING-VERTOL VR-7 WITH TAB
11. EPPLER 636
12. Horten 11.00% thick 4.00% camber
13. USA 45 M
14. NACA63-511 a=0.2
15. NACA45012
16. NACA63-611 a=0.0
17. NACA35012
18. NACA64-512 a=0.0
19. NACA35010.5
20. BOEING-VERTOL VR-7
21. NACA63-511 a=0.0