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