Similarly shaped airfoils to NACA44115
New! Bulk download of polars in Excel format: NACA44115.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. NACA35115
3. NACA44116
4. NACA44114
5. Horten 15.00% thick 4.00% camber
6. Horten 15.00% thick 5.00% camber
7. NACA35114.5
8. NACA34115
9. NACA44015
10. Horten 16.00% thick 5.00% camber
11. Horten 16.00% thick 4.00% camber
12. NACA34114.5
13. NACA35116
14. NACA45115
15. NACA44014.5
16. NACA44113.5
17. Horten 14.00% thick 4.00% camber
18. Horten 14.00% thick 5.00% camber
19. NACA35114
20. NACA45114.5
21. NACA34114