Similarly shaped airfoils to Horten 18.00% thick 5.00% camber
New! Bulk download of polars in Excel format: Horten%2018.00%25%20thick%205.00%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. Horten 19.00% thick 5.00% camber
3. Horten 17.00% thick 5.00% camber
4. Horten 18.00% thick 6.00% camber
5. NACA35118
6. NACA45117
7. NACA35117
8. Horten 17.00% thick 6.00% camber
9. Horten 19.00% thick 6.00% camber
10. NACA45119
11. NACA35119
12. NACA45018
13. NACA45116.5
14. NACA35116.5
15. Horten 18.00% thick 4.00% camber
16. NACA44018
17. NACA44118
18. Horten 17.00% thick 4.00% camber
19. NACA44117
20. NACA45017
21. NACA45019