Similarly shaped airfoils to GOE 118 (MVA MK.7)
New! Bulk download of polars in Excel format: goe118.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
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2. EPPLER 385
3. GOE 124 (MVA H.4)
4. GOE 450
5. GOE 610-B MOD.
6. GOE 428
7. GOE 610 B
8. GOE 439
9. GOE 174 (ALBATROS 5020)
10. GOE 359
11. GOE 458
12. GOE 456
13. GOE 184 (MVA H.29)
14. GOE 529
15. GOE 173 (ALBATROS 6020)
16. Eiffel 36
17. GOE 311 (MVA H.43)
18. NACA64-709 a=0.6
19. GOE 155 (SSW D.1)
20. NACA63-709 a=0.6
21. NACA64-709 a=0.5