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
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
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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