Similarly shaped airfoils to GOE 226 (MVA H.36)


New! Bulk download of polars in Excel format: goe226.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
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 73-CL3-152
2. GOE 227 (MVA H.37)
3. Joukowsky 14.00% thick 8.00% camber
4. GOE 225 (MVA H.35)
5. Joukowsky 13.00% thick 8.00% camber
6. Joukowsky 14.00% thick 9.00% camber
7. Joukowsky 15.00% thick 8.00% camber
8. Joukowsky 13.00% thick 9.00% camber
9. EPPLER 421
10. Joukowsky 15.00% thick 9.00% camber
11. Joukowsky 12.00% thick 8.00% camber
12. FX 72-MS-150A
13. GOE 441
14. GOE 242 (MVA PR.2)
15. FX 76-MP-120
16. Joukowsky 12.00% thick 9.00% camber
17. Joukowsky 16.00% thick 8.00% camber
18. FX 73-CL2-152
19. Joukowsky 16.00% thick 9.00% camber
20. MH 113 14.62%
21. HG(1)-1715