Similarly shaped airfoils to NACA45110.5
New! Bulk download of polars in Excel format: NACA45110.5.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. Horten 11.00% thick 5.00% camber
3. Horten 10.00% thick 5.00% camber
4. Horten 11.00% thick 6.00% camber
5. Horten 10.00% thick 6.00% camber
6. NACA44110.5
7. NACA35110.5
8. NACA44110
9. NACA45112
10. NACA45109
11. NACA35110
12. Horten 12.00% thick 5.00% camber
13. Horten 9.00% thick 5.00% camber
14. Horten 12.00% thick 6.00% camber
15. NACA45010.5
16. NACA45010
17. Horten 9.00% thick 6.00% camber
18. FX 77-W-121
19. NACA44010.5
20. NACA44109
21. NACA35109