Similarly shaped airfoils to GOE 602 MOD.
New! Bulk download of polars in Excel format: goe602m.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. MH 116 9.84%
3. MH 38 9.68%
4. NACA4409
5. SD7043 (9.1%)
6. HQ 3.5/10
7. EM J18 3510 26 51
8. SD7032-099-88
9. NACA4410
10. NACA63-610 a=0.8
11. PSU 94-097 (AIAA 2001-2478)
12. NACA63-710
13. HQ 3.5/9
14. RAF 32 MOD
15. SB99 F3J
16. GOE 116 (MVA MK.3)
17. EPPLER 392
18. GOE 602
19. NACA63A609
20. GOE 115 (MVA MK.2)
21. NACA63A610