Similarly shaped airfoils to GOE 767
New! Bulk download of polars in Excel format: goe767.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. HM391-1
3. MH 108 11.98%
4. OAF128
5. JWL081 11/1.3
6. HM391-2
7. Joukowsky 12.00% thick 1.00% camber
8. HM50
9. Horten 11.00% thick 2.00% camber
10. FAD04
11. Horten 11.00% thick 1.00% camber
12. Borge-b3
13. REPUBLIC S-3
14. JWL067 11.5/1.7
15. MJZ1211
16. BOEING-VERTOL V23010-1.58
17. NACA23010.5
18. Horten 12.00% thick 2.00% camber
19. Joukowsky 11.00% thick 1.00% camber
20. MH 106 13.07%
21. NACA23110.5