Similarly shaped airfoils to GOE 770
New! Bulk download of polars in Excel format: goe770.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. GOE 735
3. ARA-D 20%
4. NACA63-720 a=0.2
5. GA 30-420
6. GA 30-620
7. GA 30A420
8. GA 30A620
9. NACA64-720 a=0.2
10. AH 93-W-215
11. NACA63-720 a=0.0
12. GOE 424
13. NACA63-620 a=0.5
14. GA 30-419
15. GA 30-619
16. GOE 383
17. GA 35-420
18. GA 35A420
19. GA 30A419
20. GA 35-620
21. NACA63-620 a=0.2