Similarly shaped airfoils to NACA0015
New! Bulk download of polars in Excel format: NACA0015.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (112) | 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. GA 30A015
3. Horten 15.00% thick 0.00% camber
4. EPPLER 477
5. EPPLER 475
6. GA 30A014
7. GA 30-014
8. Horten 16.00% thick 0.00% camber
9. NACA0016
10. GA 35A015
11. NACA63-015A
12. NACA63A015
13. Horten 14.00% thick 0.00% camber
14. Horten 15.00% thick 1.00% camber
15. GA 30-016
16. GA 30A016
17. S8035 (14%)
18. GA 35A016
19. NACA63A016
20. GA 37A015
21. NACA64(2)-015A