Similarly shaped airfoils to GOE 167 (V.KARMAN PROP.2)
New! Bulk download of polars in Excel format: goe167.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 134 (MVA H.12)
3. GOE 596
4. GA 30A610
5. NACA63-710 a=0.2
6. NACA64-710 a=0.2
7. GOE 407
8. GOE 286
9. GA 30-610
10. GA 35A610
11. GOE 188
12. GOE 613
13. AQUILA 9.3% smoothed
14. USA 26
15. Fage & Collins 3
16. GA 37A610
17. NACA65-710 a=0.2
18. GOE 389
19. GOE 287
20. GOE 257
21. GA 37-610