Similarly shaped airfoils to NACA1415
New! Bulk download of polars in Excel format: NACA1415.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. NACA2415
3. NACA2315
4. NACA63A216
5. NACA2215
6. NACA64A215
7. NACA63-216
8. NACA63A115
9. NACA63-216 a=0.8
10. NACA24015
11. NACA63-215
12. NACA64-216
13. NACA63-216 a=0.6
14. NACA63-216 a=0.5
15. HAWKER TEMPEST 37.5% SEMISPAN
16. NACA64-216 a=0.8
17. NACA63-216 a=0.2
18. NACA63-215 a=0.8
19. NACA64-215
20. NACA64-216 a=0.6
21. NACA24014.5