Similarly shaped airfoils to FX 63-137 13.7% smoothed
New! Bulk download of polars in Excel format: fx63137sm.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 14.00% thick 6.00% camber
3. Joukowsky 13.00% thick 6.00% camber
4. GOE 501
5. EPPLER 396
6. Joukowsky 15.00% thick 6.00% camber
7. FX 63-120
8. GOE 497
9. EPPLER 397
10. MH 114 13.02%
11. EPPLER 395
12. Joukowsky 12.00% thick 6.00% camber
13. Joukowsky 14.00% thick 7.00% camber
14. GOE 567
15. Joukowsky 13.00% thick 7.00% camber
16. USA 98
17. MH 115 11.06%
18. Joukowsky 15.00% thick 7.00% camber
19. EPPLER 399
20. GOE 430
21. RAF 32