Similarly shaped airfoils to NACA2215
New! Bulk download of polars in Excel format: NACA2215.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (116) | 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. NACA25015
3. NACA25014.5
4. GA 30A215
5. GA 30-215
6. NACA2415
7. NACA2216
8. NACA25014
9. GA 30A214
10. GA 30-214
11. NACA63(2)A-015
12. GA 35A215
13. NACA2416
14. NACA2414
15. Horten 15.00% thick 2.00% camber
16. GA 30-216
17. NACA1415
18. GA 30A216
19. Falcon (Carl Goldberg Falcon 56 Mk II R/C powerplane)
20. NACA63-316 a=0.2
21. GOE 738