Similarly shaped airfoils to Horten 17.00% thick 5.00% camber
New! Bulk download of polars in Excel format: Horten%2017.00%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. NACA45116.5
3. Horten 18.00% thick 5.00% camber
4. Horten 16.00% thick 5.00% camber
5. Horten 17.00% thick 6.00% camber
6. NACA35117
7. NACA35116.5
8. NACA45116
9. NACA45118
10. NACA35116
11. NACA44116
12. Horten 18.00% thick 6.00% camber
13. Horten 16.00% thick 4.00% camber
14. NACA35118
15. NACA45017
16. Horten 17.00% thick 4.00% camber
17. NACA45016.5
18. NACA44017
19. NACA44116.5
20. NACA44016.5
21. NACA44117