Similarly shaped airfoils to GOE 225 (MVA H.35)
New! Bulk download of polars in Excel format: goe225.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. Joukowsky 12.00% thick 8.00% camber
3. GOE 226 (MVA H.36)
4. Joukowsky 14.00% thick 8.00% camber
5. GOE 431
6. GOE 227 (MVA H.37)
7. Joukowsky 11.00% thick 8.00% camber
8. Joukowsky 13.00% thick 7.00% camber
9. FX 76-MP-120
10. Joukowsky 12.00% thick 7.00% camber
11. Joukowsky 15.00% thick 8.00% camber
12. Joukowsky 13.00% thick 9.00% camber
13. Joukowsky 14.00% thick 7.00% camber
14. FX 73-CL3-152
15. Joukowsky 12.00% thick 9.00% camber
16. Joukowsky 14.00% thick 9.00% camber
17. MH 114 13.02%
18. Joukowsky 11.00% thick 7.00% camber
19. FX 73-CL2-152
20. MID 405e
21. MID 405w2