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
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. 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