Similarly shaped airfoils to GOE 228 (MVA H.38)
New! Bulk download of polars in Excel format: goe228.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 222 (MVA H.33)
3. Joukowsky 18.00% thick 8.00% camber
4. Joukowsky 17.00% thick 8.00% camber
5. Joukowsky 19.00% thick 8.00% camber
6. Joukowsky 18.00% thick 7.00% camber
7. Joukowsky 17.00% thick 7.00% camber
8. Joukowsky 19.00% thick 7.00% camber
9. GOE 441
10. Joukowsky 16.00% thick 8.00% camber
11. MH 113 14.62%
12. EPPLER 591
13. GOE 422
14. Joukowsky 16.00% thick 7.00% camber
15. FX 76-MP-160
16. Joukowsky 20.00% thick 8.00% camber
17. GOE 217 (MVA MK.12)
18. GOE 614
19. GOE 229 (MVA H.39)
20. USA 34
21. GOE 223 (MVA H.34)