Similarly shaped airfoils to GOE 531
New! Bulk download of polars in Excel format: goe531.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. EPPLER 420
3. CH10 (smoothed)
4. GOE 244 (MVA PR.4)
5. GOE 523
6. GOE 525
7. EPPLER 423
8. FX 72-MS-150B
9. GOE 440
10. Joukowsky 14.00% thick 10.00% camber
11. Joukowsky 15.00% thick 10.00% camber
12. Joukowsky 13.00% thick 10.00% camber
13. Joukowsky 16.00% thick 10.00% camber
14. FX 74-Cl5-140 MOD (smoothed)
15. FX 74_CL5_140
16. S9104
17. Joukowsky 12.00% thick 10.00% camber
18. Joukowsky 17.00% thick 10.00% camber
19. S9104BTE
20. Joukowsky 11.00% thick 10.00% camber
21. Joukowsky 18.00% thick 10.00% camber