Similarly shaped airfoils to NACA45015
New! Bulk download of polars in Excel format: NACA45015.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. NACA35014.5
3. NACA44015
4. NACA44014.5
5. NACA45016
6. NACA35114.5
7. NACA45014.5
8. Horten 15.00% thick 4.00% camber
9. NACA35014
10. NACA35016
11. NACA44014
12. NACA35115
13. NACA35114
14. NACA44016
15. NACA34014.5
16. EPPLER 342
17. NACA45014
18. NACA34014
19. NACA45016.5
20. Horten 14.00% thick 4.00% camber
21. Horten 16.00% thick 4.00% camber