Similarly shaped airfoils to GOE 502
New! Bulk download of polars in Excel format: goe502.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 16.00% thick 6.00% camber
3. Joukowsky 17.00% thick 6.00% camber
4. Joukowsky 16.00% thick 7.00% camber
5. Joukowsky 17.00% thick 7.00% camber
6. Joukowsky 15.00% thick 6.00% camber
7. GOE 675
8. DOUGLAS LA203A
9. MID 406w2
10. FX 76-MP-160
11. GOE 288
12. GOE 535
13. GOE 628
14. USA 98
15. GOE 289 (MVA 289)
16. Joukowsky 18.00% thick 6.00% camber
17. EPPLER 561
18. Joukowsky 15.00% thick 7.00% camber
19. Joukowsky 18.00% thick 7.00% camber
20. GOE 481A
21. GOE 567