Similarly shaped airfoils to SG6041_PSO
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. NACA63A610
3. RAF 32 MOD
4. NACA64A610
5. HQ 3.5/10
6. MH 116 9.84%
7. GOE 547
8. NACA64-611 a=0.8
9. NACA63A611
10. GOE 546
11. NACA65-610 a=0.8
12. EPPLER 66
13. NACA65-710
14. NACA64-610 a=0.8
15. NACA64-711
16. NACA64A611
17. NACA64-710
18. NACA65A610
19. NACA63-611 a=0.8
20. PSU 94-097 (AIAA 2001-2478)
21. NACA63-610 a=0.8