Similarly shaped airfoils to NACA44110.5
New! Bulk download of polars in Excel format: NACA44110.5.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. NACA35110.5
3. NACA35110
4. Horten 11.00% thick 5.00% camber
5. Horten 10.00% thick 5.00% camber
6. NACA34110.5
7. NACA44010.5
8. NACA34110
9. NACA45110.5
10. NACA44010
11. Horten 10.00% thick 4.00% camber
12. Horten 11.00% thick 4.00% camber
13. NACA44109
14. NACA45110
15. NACA45010.5
16. Horten 12.00% thick 5.00% camber
17. NACA35109
18. NACA35112
19. NACA44112
20. NACA45010
21. Horten 9.00% thick 5.00% camber