Similarly shaped airfoils to Horten 12.00% thick 3.00% camber


New! Bulk download of polars in Excel format: Horten%2012.00%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. EH 3.0/12
2. NACA25112
3. NACA34012
4. NACA33012
5. EPPLER 636
6. CLARK YS
7. Horten 11.00% thick 3.00% camber
8. EPPLER 331
9. EPPLER 635
10. EPPLER 332
11. Horten 12.00% thick 4.00% camber
12. NACA34112
13. NACA 2R212
14. NACA25113
15. EH 2.0/12
16. M-35A-12.7
17. EPPLER 336
18. MARSKE PIONEER IID ROOT (NACA 431012A/24112 HYBRID)
19. NACA35012
20. Horten 13.00% thick 3.00% camber
21. NACA34013