Similarly shaped airfoils to NACA33014.5
New! Bulk download of polars in Excel format: NACA33014.5.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. NACA33014
3. NACA33114.5
4. NACA24114.5
5. NACA25114.5
6. NACA33114
7. NACA24114
8. NACA33115
9. NACA25115
10. NACA25114
11. NACA24115
12. NACA33013.5
13. NACA34015
14. NACA24014.5
15. Horten 15.00% thick 2.00% camber
16. NACA32014.5
17. NACA42013.5
18. NACA32014
19. Horten 15.00% thick 3.00% camber
20. Horten 14.00% thick 2.00% camber
21. NACA24014