Similarly shaped airfoils to GOE 241 (MVA PR.1)


New! Bulk download of polars in Excel format: goe241.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 243 (MVA PR.3)
2. Joukowsky 18.00% thick 9.00% camber
3. Joukowsky 19.00% thick 9.00% camber
4. GOE 482
5. Joukowsky 17.00% thick 9.00% camber
6. Joukowsky 18.00% thick 10.00% camber
7. Joukowsky 19.00% thick 10.00% camber
8. Joukowsky 20.00% thick 9.00% camber
9. Joukowsky 17.00% thick 10.00% camber
10. Joukowsky 20.00% thick 10.00% camber
11. Joukowsky 16.00% thick 9.00% camber
12. GOE 441
13. MH 112 16.2%
14. Joukowsky 18.00% thick 8.00% camber
15. GOE 228 (MVA H.38)
16. Joukowsky 19.00% thick 8.00% camber
17. Joukowsky 17.00% thick 8.00% camber
18. Joukowsky 16.00% thick 10.00% camber
19. GOE 244 (MVA PR.4)
20. GOE 525
21. GOE 523