Similarly shaped airfoils to NACA45116.5
New! Bulk download of polars in Excel format: NACA45116.5.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
3. Horten 17.00% thick 5.00% camber
4. Horten 16.00% thick 5.00% camber
5. Horten 17.00% thick 6.00% camber
6. Horten 16.00% thick 6.00% camber
7. NACA44116
8. NACA45118
9. NACA45115
10. NACA35116.5
11. NACA35116
12. NACA35117
13. Horten 16.00% thick 4.00% camber
14. Horten 18.00% thick 5.00% camber
15. Horten 15.00% thick 5.00% camber
16. NACA45016.5
17. Horten 18.00% thick 6.00% camber
18. NACA45017
19. NACA45016
20. NACA44115
21. NACA45114.5