Similarly shaped airfoils to GOE 222 (MVA H.33)


New! Bulk download of polars in Excel format: goe222.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. GOE 228 (MVA H.38)
2. Joukowsky 19.00% thick 8.00% camber
3. Joukowsky 18.00% thick 8.00% camber
4. Joukowsky 19.00% thick 7.00% camber
5. Joukowsky 18.00% thick 7.00% camber
6. MH 112 16.2%
7. Joukowsky 20.00% thick 8.00% camber
8. GOE 229 (MVA H.39)
9. Joukowsky 17.00% thick 8.00% camber
10. Joukowsky 20.00% thick 7.00% camber
11. GOE 614
12. Joukowsky 17.00% thick 7.00% camber
13. GOE 422
14. GOE 223 (MVA H.34)
15. FX 76-MP-160
16. GOE 620
17. USA 34
18. GOE 421
19. Joukowsky 19.00% thick 9.00% camber
20. Joukowsky 16.00% thick 8.00% camber
21. Joukowsky 18.00% thick 9.00% camber