Similarly shaped airfoils to GOE 600
New! Bulk download of polars in Excel format: goe600.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. NACA63A313
3. GA 30-213
4. GA 35A213
5. NACA63A314
6. GA 35A214
7. NACA64A313
8. RAF 31
9. GA 37A213
10. NACA64A314
11. Jedeslsky EJ1
12. GA 37A214
13. MS(1)-0313
14. NACA64-314 a=0.8
15. NACA64-314 a=0.6
16. EPPLER 209
17. NACA64-414
18. GA 37-214
19. LS(1)-0413MOD
20. NACA64-314 a=0.5
21. NACA63-314 a=0.8