Similarly shaped airfoils to NACA45110
New! Bulk download of polars in Excel format: NACA45110.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
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2. Horten 10.00% thick 5.00% camber
3. NACA45109
4. Horten 10.00% thick 6.00% camber
5. Horten 11.00% thick 5.00% camber
6. Horten 9.00% thick 5.00% camber
7. Horten 11.00% thick 6.00% camber
8. NACA44110
9. NACA35110
10. Horten 9.00% thick 6.00% camber
11. NACA44110.5
12. NACA35110.5
13. NACA45010
14. NACA44109
15. NACA35109
16. NACA45010.5
17. NACA45009
18. GOE 746
19. NACA45112
20. NACA 6-H-10
21. NACA44010