Similarly shaped airfoils to GOE 703
New! Bulk download of polars in Excel format: goe703.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. GA 30A220
3. TsAGI B 19.0% thick
4. GA 35A220
5. GA 30-220
6. TsAGI B 19.5% thick
7. GA 37A220
8. TsAGI B 18.5% thick
9. GA 30A219
10. TsAGI B 20.0% thick
11. GA 30-219
12. NACA2321
13. NACA35019
14. GA 30A320
15. TsAGI B 18.0% thick
16. NACA35021
17. NACA65-420 a=0.2
18. GA 35A320
19. NACA65-420 a=0.0
20. GA 30-320
21. RAF 69