Similarly shaped airfoils to GOE 525
New! Bulk download of polars in Excel format: goe525.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. GOE 244 (MVA PR.4)
3. Joukowsky 16.00% thick 10.00% camber
4. Joukowsky 17.00% thick 10.00% camber
5. Joukowsky 15.00% thick 10.00% camber
6. FX 72-MS-150B
7. Joukowsky 18.00% thick 10.00% camber
8. EPPLER 420
9. GOE 440
10. Joukowsky 14.00% thick 10.00% camber
11. GOE 482
12. CH10 (smoothed)
13. GOE 241 (MVA PR.1)
14. Joukowsky 19.00% thick 10.00% camber
15. FX 74_CL5_140
16. Joukowsky 16.00% thick 9.00% camber
17. Joukowsky 13.00% thick 10.00% camber
18. EPPLER 423
19. GOE 243 (MVA PR.3)
20. Joukowsky 15.00% thick 9.00% camber
21. Joukowsky 17.00% thick 9.00% camber