Similarly shaped airfoils to GOE 704
New! Bulk download of polars in Excel format: goe704.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. TsAGI B 13.5% thick
3. TsAGI B 12.5% thick
4. GOE 617
5. TsAGI B 14.0% thick
6. NACA25013.5
7. GA 30A213
8. ONERA OA212
9. GA 30A214
10. RC-12(B)3
11. NACA25014
12. NACA2213
13. NACA25013
14. NACA M6
15. Falcon (Carl Goldberg Falcon 56 Mk II R/C powerplane)
16. GA 30-213
17. GOE 677 (= M 6)
18. GA 30-214
19. NACA25113.5
20. RAF 34
21. GA 35A214