Similarly shaped airfoils to GOE 766
New! Bulk download of polars in Excel format: goe766.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. MJZ1211
3. HM391-1
4. NACA23012
5. NACA24012
6. GOE 767
7. MH 108 11.98%
8. ONERA NACA CAMBRE
9. Borge-b3
10. NACA23112
11. Horten 11.00% thick 2.00% camber
12. NACA24112
13. EH 2.0/12
14. MH 106 13.07%
15. Horten 11.00% thick 1.00% camber
16. NACA32012
17. Ritz 1-30-12
18. JWL081 11/1.3
19. NPL 9627
20. JWL067 11.5/1.7
21. NACA25012