Similarly shaped airfoils to NACA44116
New! Bulk download of polars in Excel format: NACA44116.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. NACA44115
3. Horten 16.00% thick 4.00% camber
4. Horten 16.00% thick 5.00% camber
5. NACA35116.5
6. NACA44116.5
7. NACA34116
8. NACA44016
9. Horten 17.00% thick 5.00% camber
10. NACA35115
11. NACA35117
12. NACA44016.5
13. NACA45116
14. NACA34116.5
15. NACA45116.5
16. NACA44114.5
17. Horten 15.00% thick 4.00% camber
18. Horten 15.00% thick 5.00% camber
19. NACA34115
20. NACA44117
21. NACA44017