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
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. 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