Similarly shaped airfoils to S4320
New! Bulk download of polars in Excel format: s4320.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. S2091-101-83
3. GOE 180 (MVA H.26)
4. GA 35-610
5. USA 22
6. GOE 178
7. S4062-095-87
8. GOE 277 (DAIMLER VIII)
9. SD7032-099-88
10. SD7034
11. DAE-51
12. EPPLER 392
13. GOE 287
14. NACA63-709 a=0.5
15. GA 37-610
16. SD7043 (9.1%)
17. GOE 328
18. GOE 117 (MVA MK.4)
19. PSU 94-097 (AIAA 2001-2478)
20. NACA63-609 a=0.5
21. GOE 326 (PFALZ 55)