Similarly shaped airfoils to Horten 14.00% thick 4.00% camber
New! Bulk download of polars in Excel format: Horten%2014.00%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. NACA44014
3. NACA35113.5
4. Horten 15.00% thick 4.00% camber
5. Horten 13.00% thick 4.00% camber
6. NACA35114.5
7. NACA44114
8. NACA44013.5
9. Horten 14.00% thick 5.00% camber
10. NACA44113.5
11. NACA44014.5
12. EPPLER 342
13. NACA34113
14. NACA44114.5
15. EPPLER 625
16. NACA35115
17. EPPLER 341
18. NACA34114
19. NACA34113.5
20. NACA35113
21. NACA34014