Similarly shaped airfoils to NACA63-714
New! Bulk download of polars in Excel format: NACA63-714.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. NACA63-614 a=0.8
3. NACA64-614 a=0.8
4. FX 75-141
5. HQ 3.5/14
6. NACA63-715
7. NACA63-713
8. HQ 3.5/13
9. EPPLER 68
10. EPPLER 854
11. NACA64-713
12. NACA63(2)-615
13. NACA64-715
14. NACA63A614
15. NACA63-514 a=0.8
16. NACA63-615 a=0.8
17. HQ 3.0/14
18. NACA63-614
19. NACA63-613 a=0.8
20. NACA64-514 a=0.8
21. NACA64-615 a=0.8