Similarly shaped airfoils to NACA0013
New! Bulk download of polars in Excel format: NACA0013.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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. GA 30A013
3. Horten 13.00% thick 0.00% camber
4. GOE 459
5. RAF 30
6. GOE 409
7. St. CYR 172 (Royer)
8. FX 76-120
9. GA 30A012
10. GA 35A013
11. NACA63A013
12. GA 30-012
13. S8035 (14%)
14. J5012 12%
15. NACA M3
16. Horten 14.00% thick 0.00% camber
17. NACA0012
18. LS(1)-0013
19. Ultimate (Carl Goldberg Ultimate Bipe R/C)
20. Horten 12.00% thick 0.00% camber
21. SC(2)-0012