Similarly shaped airfoils to GOE 358


New! Bulk download of polars in Excel format: goe358.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. Joukowsky 10.00% thick 6.00% camber
2. GOE 165 (MVA MK.11)
3. Joukowsky 11.00% thick 6.00% camber
4. Joukowsky 9.00% thick 6.00% camber
5. GOE 500
6. GOE 496
7. GOE 190 (MVA MK.18)
8. Joukowsky 10.00% thick 5.00% camber
9. GOE 176 (ALBATROS 7020)
10. Joukowsky 9.00% thick 5.00% camber
11. Joukowsky 11.00% thick 5.00% camber
12. GOE 195
13. EPPLER 216
14. Joukowsky 12.00% thick 6.00% camber
15. GOE 239 (MVA H.31)
16. EPPLER 385
17. SG6043
18. NACA6409
19. HL73-650
20. MH 115 11.06%
21. NACA6410