Similarly shaped airfoils to PSU 94-097 (AIAA 2001-2478)
New! Bulk download of polars in Excel format: psu94097.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. S4062-095-87
3. DAE-51
4. EPPLER 392
5. SD7032-099-88
6. GOE 602 MOD.
7. GA 35A610
8. GA 30-610
9. NACA63-610 a=0.6
10. GA 35-610
11. MH 38 9.68%
12. NACA64-610 a=0.6
13. GA 37-610
14. GA 30A610
15. RAF 32 MOD
16. GA 37A610
17. HQ 3.5/10
18. NACA63-610 a=0.8
19. EPPLER 66
20. NACA63A710
21. NACA64-610 a=0.8