Similarly shaped airfoils to Horten 11.00% thick 3.00% camber


New! Bulk download of polars in Excel format: Horten%2011.00%25%20thick%203.00%25%20camber.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. NACA25110.5
2. EPPLER 331
3. EH 3.0/12
4. EPPLER 635
5. Horten 12.00% thick 3.00% camber
6. Horten 10.00% thick 3.00% camber
7. NACA33010.5
8. NACA34010.5
9. EPPLER 636
10. EPPLER 332
11. NACA25110
12. NACA33110.5
13. Horten 11.00% thick 4.00% camber
14. NACA25112
15. NACA24110.5
16. EH 2.5/10
17. RC_Milan
18. NACA34110.5
19. NACA33010
20. RC(4)-10
21. NACA34012