Similarly shaped airfoils to Horten 9.00% thick 4.00% camber


New! Bulk download of polars in Excel format: Horten%209.00%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. NACA35109
2. NACA34109
3. NACA44109
4. NACA44009
5. NACA35110
6. Horten 10.00% thick 4.00% camber
7. Horten 9.00% thick 5.00% camber
8. NACA35009
9. HS 3.0/9.0
10. NACA34009
11. NACA45009
12. NACA44010
13. NACA34110
14. NACA44110
15. Horten 10.00% thick 5.00% camber
16. NACA35010
17. NACA35110.5
18. Horten 9.00% thick 3.00% camber
19. Phoenix10
20. FAD23
21. HS 3.0/8