Similarly shaped airfoils to Horten 10.00% thick 4.00% camber


New! Bulk download of polars in Excel format: Horten%2010.00%25%20thick%204.00%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. NACA34110
2. NACA35110
3. NACA34110.5
4. NACA35110.5
5. Horten 11.00% thick 4.00% camber
6. NACA34109
7. Horten 10.00% thick 3.00% camber
8. Horten 9.00% thick 4.00% camber
9. NACA34010
10. Phoenix10
11. NACA35010
12. NACA35109
13. FAD23
14. NACA35010.5
15. NACA34010.5
16. NACA44110
17. NACA44010
18. NACA44110.5
19. NACA44010.5
20. Horten 9.00% thick 3.00% camber
21. Horten 11.00% thick 3.00% camber