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
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 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