Similarly shaped airfoils to GOE 567
New! Bulk download of polars in Excel format: goe567.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. Joukowsky 15.00% thick 5.00% camber
3. EPPLER 397
4. Joukowsky 14.00% thick 5.00% camber
5. EPPLER 560
6. Joukowsky 15.00% thick 6.00% camber
7. GOE 430
8. EPPLER 396
9. Joukowsky 16.00% thick 5.00% camber
10. MID 403
11. Joukowsky 14.00% thick 6.00% camber
12. GOE 626
13. GOE 497
14. Joukowsky 16.00% thick 6.00% camber
15. EPPLER 559
16. RAF 32
17. GOE 619
18. GOE 612
19. GOE 621
20. GOE 498
21. EPPLER 793