Similarly shaped airfoils to NACA44116.5
New! Bulk download of polars in Excel format: NACA44116.5.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
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2. NACA34116.5
3. NACA34117
4. NACA34116
5. Horten 17.00% thick 4.00% camber
6. NACA35116.5
7. NACA35117
8. NACA44116
9. NACA35116
10. NACA44118
11. NACA34118
12. Horten 18.00% thick 4.00% camber
13. Horten 16.00% thick 4.00% camber
14. NACA34115
15. Horten 17.00% thick 5.00% camber
16. NACA35118
17. NACA44016.5
18. Horten 17.00% thick 3.00% camber
19. NACA34016.5
20. NACA44017
21. NACA33116.5