Similarly shaped airfoils to GOE 599


New! Bulk download of polars in Excel format: goe599.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
Dynamic plotter New!
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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1. AIR 100-2 Acro MM 576 1999
2. EM CY 1016 1510
3. NACA63A210
4. NACA64A210
5. RG 14 10%
6. NACA63A310
7. NACA65A210
8. SB96VS 9.75/1.25
9. NACA65-310
10. NACA0010-34 a=0.8 c(li)=0.2
11. NACA64A310
12. GA 30A210
13. TPR-95-96-95
14. HQ 1.5/10
15. NACA63A211
16. RG 14 9.5%
17. NACA64-311
18. NACA64A211
19. SG6041
20. RAF 28
21. GA 35A210