Similarly shaped airfoils to GOE 548
New! Bulk download of polars in Excel format: goe548.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. NACA63A412
3. NACA65A412
4. NACA64A413
5. NACA63A413
6. LOCKHEED L-188 TIP
7. PSU-90-125WL
8. NACA65(1)-412
9. NACA65-412
10. AMSOIL1 RUTAN CANARD
11. NACA65-412 a=0.8
12. NACA65A312
13. GA 37A312
14. NACA65A413
15. EM CY 1016 2012
16. NACA64A312
17. RAF 31
18. LDS-2
19. NACA65-413 a=0.8
20. GA 35A312
21. NACA65-413