Similarly shaped airfoils to GOE 571
New! Bulk download of polars in Excel format: goe571.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. GOE 384
8. USA 34
9. GOE 625
10. GOE 511
11. GU25-5(11)8
12. Marsden
13. GOE 798
14. Joukowsky 20.00% thick 10.00% camber
15. GOE 777
16. GOE 382
17. Joukowsky 20.00% thick 9.00% camber
18. UA(2)-180 smoothed
19. GOE 241 (MVA PR.1)
20. Joukowsky 20.00% thick 8.00% camber
21. Joukowsky 19.00% thick 10.00% camber