Similarly shaped airfoils to Fage & Collins 3
New! Bulk download of polars in Excel format: fg3.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. USA 26
3. GOE 385
4. GOE 167 (V.KARMAN PROP.2)
5. GOE 134 (MVA H.12)
6. ARA-D 10%
7. GOE 407
8. NACA65-711 a=0.2
9. GOE 389
10. GA 30A610
11. NACA64-711 a=0.2
12. NACA65-710 a=0.2
13. GOE 596
14. NACA66-710 a=0.2
15. GA 30A611
16. S4310
17. GA 35A611
18. GA 37A611
19. GOE 574
20. GOE 436
21. GA 30-610