Similarly shaped airfoils to GOE 501
New! Bulk download of polars in Excel format: goe501.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. MH 114 13.02%
3. Joukowsky 13.00% thick 6.00% camber
4. Joukowsky 14.00% thick 7.00% camber
5. FX 63-137
6. FX 63-137 13.7% smoothed
7. Joukowsky 12.00% thick 7.00% camber
8. Joukowsky 14.00% thick 6.00% camber
9. Joukowsky 12.00% thick 6.00% camber
10. MID 405w2
11. MID 405e
12. DAE-21
13. DAE-31
14. USA 98
15. DAE-11
16. MH 115 11.06%
17. GOE 239 (MVA H.31)
18. EPPLER 396
19. Joukowsky 15.00% thick 7.00% camber
20. GOE 446
21. GOE 332 (PFALZ 61)