Similarly shaped airfoils to FX 60-126/1
New! Bulk download of polars in Excel format: fx601261.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. Joukowsky 12.00% thick 4.00% camber
3. Joukowsky 13.00% thick 4.00% camber
4. NM Retro 13
5. MS535-3V
6. EPPLER 393
7. GOE 550
8. NACA63-612 a=0.8
9. GOE 685
10. GOE 723
11. NACA63-712
12. HQ 3.5/12
13. Joukowsky 11.00% thick 4.00% camber
14. EPPLER 214
15. FX 83-W-108
16. JWL041 11/3.5
17. NM Retro 14
18. EPPLER 67
19. Joukowsky 14.00% thick 4.00% camber
20. EM J18 3212
21. NACA63-712 a=0.8