Similarly shaped airfoils to SG6043
New! Bulk download of polars in Excel format: sg6043.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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. NACA6410
3. GOE 500
4. EPPLER 216
5. NACA6409
6. GOE 239 (MVA H.31)
7. Joukowsky 11.00% thick 6.00% camber
8. FX 63-120
9. GOE 496
10. Joukowsky 10.00% thick 6.00% camber
11. GOE 450
12. GOE 330 (PFALZ 59)
13. GOE 303 (FRIEDRICHSHAFEN G03)
14. NACA5510
15. GOE 477
16. GOE 392
17. GOE 176 (ALBATROS 7020)
18. Joukowsky 12.00% thick 6.00% camber
19. GOE 282 (DAIMLER XIII)
20. EPPLER 395
21. GOE 529