Similarly shaped airfoils to GOE 746
New! Bulk download of polars in Excel format: goe746.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. GOE 318 (HANSA-BRANDENBURG VI.5)
3. Horten 9.00% thick 6.00% camber
4. NACA45109
5. EPPLER 593
6. Horten 10.00% thick 6.00% camber
7. EPPLER 598
8. LISSAMAN 7769
9. GOE 316 (HANSA-BRANDENBURG IV.5)
10. NACA45110
11. Horten 9.00% thick 5.00% camber
12. NACA63-709 a=0.2
13. NACA63-710 a=0.2
14. NACA63-709 a=0.0
15. NACA 6-H-10
16. NACA63-710 a=0.0
17. NACA64-709 a=0.2
18. GOE 309 (MVA H.41)
19. NACA64-709 a=0.0
20. NACA64-710 a=0.2
21. NACA45009