Similarly shaped airfoils to GOE 223 (MVA H.34)


New! Bulk download of polars in Excel format: goe223.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 229 (MVA H.39)
2. GOE 620
3. Joukowsky 19.00% thick 6.00% camber
4. Joukowsky 18.00% thick 6.00% camber
5. GOE 614
6. GOE 288
7. FX 76-MP-160
8. EPPLER 857
9. GOE 289 (MVA 289)
10. Joukowsky 19.00% thick 7.00% camber
11. Joukowsky 20.00% thick 6.00% camber
12. Joukowsky 17.00% thick 6.00% camber
13. Joukowsky 18.00% thick 7.00% camber
14. GOE 498
15. GOE 504
16. EPPLER 748
17. GOE 502
18. Joukowsky 20.00% thick 7.00% camber
19. EPPLER 561
20. GOE 628
21. DOUGLAS LA203A