Similarly shaped airfoils to NACA44114.5
New! Bulk download of polars in Excel format: NACA44114.5.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. NACA44114
3. NACA44113.5
4. NACA35115
5. NACA35114.5
6. Horten 15.00% thick 4.00% camber
7. Horten 15.00% thick 5.00% camber
8. Horten 14.00% thick 4.00% camber
9. Horten 14.00% thick 5.00% camber
10. NACA35114
11. NACA34114.5
12. NACA44014.5
13. NACA34114
14. NACA44015
15. NACA45114.5
16. NACA44014
17. NACA34115
18. NACA45115
19. NACA44116
20. NACA44113
21. EPPLER 342