Similarly shaped airfoils to GOE 741
New! Bulk download of polars in Excel format: goe741.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 P-II (15.5%) smoothed
3. TsAGI R3A-15
4. TsAGI P-II (15.5%)
5. AUGUST 160
6. TsAGI R-II-14
7. USA 45
8. EPPLER 344
9. USA 33
10. GOE 633
11. NACA63-715 a=0.2
12. NACA63-716 a=0.2
13. Fraser_f4fras15
14. AH 80-140
15. NACA63-715 a=0.0
16. Horten 15.00% thick 6.00% camber
17. NACA63-716 a=0.0
18. Horten 14.00% thick 6.00% camber
19. NACA45014.5
20. NACA64-715 a=0.2
21. EPPLER 343