Similarly shaped airfoils to GOE 190 (MVA MK.18)


New! Bulk download of polars in Excel format: goe190.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 165 (MVA MK.11)
2. Joukowsky 12.00% thick 6.00% camber
3. Joukowsky 11.00% thick 6.00% camber
4. GOE 358
5. Joukowsky 13.00% thick 6.00% camber
6. GOE 239 (MVA H.31)
7. FX 63-120
8. MH 115 11.06%
9. Joukowsky 10.00% thick 6.00% camber
10. GOE 500
11. GOE 497
12. Joukowsky 12.00% thick 5.00% camber
13. GOE 501
14. Joukowsky 11.00% thick 5.00% camber
15. Joukowsky 12.00% thick 7.00% camber
16. Joukowsky 14.00% thick 6.00% camber
17. SG6043
18. GOE 496
19. GOE 176 (ALBATROS 7020)
20. EPPLER 395
21. EPPLER 216