Similarly shaped airfoils to Horten 12.00% thick 4.00% camber


New! Bulk download of polars in Excel format: Horten%2012.00%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

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

1. M-35A-12.7
2. NACA34112
3. EPPLER 636
4. NACA35112
5. Horten 13.00% thick 4.00% camber
6. Horten 11.00% thick 4.00% camber
7. NACA44112
8. HS 3.5/12
9. EH 3.0/12
10. Horten 12.00% thick 3.00% camber
11. EPPLER 332
12. HS 3.4.12b
13. EPPLER 637
14. NACA34012
15. NACA35012
16. NACA34113
17. NACA35113
18. NACA44013
19. EPPLER 635
20. NACA44012
21. NACA44113