Similarly shaped airfoils to NACA0016
New! Bulk download of polars in Excel format: NACA0016.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (7) | 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 30A016
3. Horten 16.00% thick 0.00% camber
4. GA 30A015
5. GA 30-015
6. Horten 17.00% thick 0.00% camber
7. NACA0015
8. NACA0017
9. EPPLER 476
10. GA 35A016
11. Horten 16.00% thick 1.00% camber
12. NACA63A016
13. Horten 15.00% thick 0.00% camber
14. GA 30-017
15. GA 30A017
16. EPPLER 477
17. NACA22016
18. GA 35A017
19. NACA63A017
20. GA 37A016
21. EPPLER 475