Similarly shaped airfoils to NACA63-015
New! Bulk download of polars in Excel format: NACA63-015.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (13) | 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. NACA64-015
3. GA 37-015
4. FX 71-L-150/25
5. FX 71-L-150/30
6. FX 71-L-150/20
7. EPPLER 477
8. NACA63-115 a=0.0
9. NACA63-115
10. NACA64-115 a=0.0
11. GA 35-014
12. GA 35-016
13. NACA63-115 a=0.2
14. NACA64-115
15. GA 37-014
16. GA 35A015
17. NACA63-015A
18. NACA63A015
19. NACA64-115 a=0.2
20. GA 37-016
21. GA 35A014