Similarly shaped airfoils to GOE 573


New! Bulk download of polars in Excel format: goe573.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
Dynamic plotter New!
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.

1. GOE 562
2. GOE 611
3. GOE 322 (HANSA-BRANDENBURG IV.1)
4. GOE 320 (HANSA-BRANDENBURG II.1)
5. GOE 615
6. GOE 512
7. GOE 510
8. GOE 505
9. GOE 387
10. NACA M24 (NACA-TR-221)
11. Glenn Martin 2
12. GOE 406
13. GOE 528
14. GOE 446
15. GOE 332 (PFALZ 61)
16. GOE 654
17. FX 049-915
18. NACA M21 (NACA-TR-221)
19. NACA M21
20. GOE 414
21. GOE 324 (HANSA-BRANDENBURG)