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
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. 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