Similarly shaped airfoils to FX 60-126
New! Bulk download of polars in Excel format: fx60126.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. MS535-3V
3. Joukowsky 12.00% thick 4.00% camber
4. Joukowsky 13.00% thick 4.00% camber
5. EM J18 3212
6. EM L3 3012
7. NACA63-712
8. EM J18 3012 DrW r1,2
9. SB96 11.6/3.0
10. NACA63-612 a=0.8
11. HQ 3.5/12
12. JWL041 11/3.5
13. SB 96 12.7/3.0
14. EPPLER 393
15. EPPLER 67
16. NACA63-713
17. Joukowsky 11.00% thick 4.00% camber
18. Joukowsky 12.00% thick 3.00% camber
19. NACA63-512 a=0.8
20. NACA64-712
21. NACA63-612