Similarly shaped airfoils to GOE 290 (MVA 290)
New! Bulk download of polars in Excel format: goe290.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 1230
3. AH 93-W-174
4. GOE 681
5. GA 30-417
6. GA 30A417
7. Pegase coap
8. NACA4416
9. GA 30-617
10. GA 30A617
11. GA 30A416
12. GA 30-416
13. CLARK YM-18
14. NACA63-618 a=0.5
15. GA 30-418
16. GA 30A616
17. GA 30-616
18. GA 30A418
19. FX 66-17AII-182
20. NACA63-618 a=0.6
21. HQ 3.5/18