Similarly shaped airfoils to GOE 561
New! Bulk download of polars in Excel format: goe561.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. KENNEDY AND MARSDEN
3. GOE 421
4. GOE 390
5. GOE 572
6. GOE 518
7. USA 34
8. GOE 384
9. GOE 511
10. GU25-5(11)8
11. GOE 625
12. Marsden
13. GOE 798
14. Joukowsky 20.00% thick 10.00% camber
15. GOE 570
16. UA(2)-180 smoothed
17. GOE 777
18. Joukowsky 20.00% thick 9.00% camber
19. GOE 382
20. GOE 241 (MVA PR.1)
21. Joukowsky 19.00% thick 10.00% camber