Similarly shaped airfoils to FX 62-K-131
New! Bulk download of polars in Excel format: fx62k131.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. NACA64A713
3. NACA65-713
4. NACA65-613 a=0.8
5. AH 88-K-130/20
6. NACA63A713
7. NACA64-713 a=0.8
8. NACA65A713
9. NACA65-714 a=0.8
10. NACA64-714 a=0.8
11. NACA64-713
12. NACA64-613 a=0.8
13. NACA63-713 a=0.8
14. NACA64A714
15. NACA65-714
16. NACA65-614 a=0.8
17. NACA64A613
18. EPPLER 668
19. NACA66A713
20. NACA65A712
21. NACA64A712