Similarly shaped airfoils to Horten 16.00% thick 3.00% camber


Direct link: Horten 16.00% thick 3.00% camber
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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1. NACA25116
2. NACA34016
3. NACA25116.5
4. NACA34016.5
5. Horten 17.00% thick 3.00% camber
6. Horten 15.00% thick 3.00% camber
7. Horten 16.00% thick 2.00% camber
8. NACA33016
9. NACA25115
10. NACA34116
11. NACA34015
12. NACA33116
13. NACA33016.5
14. NACA24116
15. NACA34116.5
16. NACA25117
17. NACA34017
18. NACA33015
19. NACA25016
20. NACA33116.5
21. NACA24116.5