Similarly shaped airfoils to FX 63-137


New! Bulk download of polars in Excel format: fx63137.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (24) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Dynamic plotter New!
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.

1. FX 63-137 13.7% smoothed
2. GOE 501
3. MH 114 13.02%
4. Joukowsky 14.00% thick 6.00% camber
5. Joukowsky 14.00% thick 7.00% camber
6. Joukowsky 13.00% thick 6.00% camber
7. Joukowsky 13.00% thick 7.00% camber
8. EPPLER 396
9. Joukowsky 15.00% thick 7.00% camber
10. Joukowsky 15.00% thick 6.00% camber
11. USA 98
12. FX 63-120
13. Joukowsky 12.00% thick 6.00% camber
14. FX 73-CL2-152
15. Joukowsky 12.00% thick 7.00% camber
16. EPPLER 591
17. GOE 497
18. EPPLER 397
19. EPPLER 395
20. MH 115 11.06%
21. MID 405e