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
Dynamic plotter New!
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.

1. GOE 448
2. EPPLER 420
3. BE183-176 (inverted)
4. CH10 (smoothed)
5. ISHAAN_001
6. GOE 244 (MVA PR.4)
7. GOE 525
8. GOE 523
9. EPPLER 423
10. FX 72-MS-150B
11. GOE 440
12. Joukowsky 14.00% thick 10.00% camber
13. Joukowsky 15.00% thick 10.00% camber
14. Joukowsky 13.00% thick 10.00% camber
15. Joukowsky 16.00% thick 10.00% camber
16. FX 74-Cl5-140 MOD (smoothed)
17. FX 74_CL5_140
18. S9104
19. Joukowsky 12.00% thick 10.00% camber
20. Joukowsky 17.00% thick 10.00% camber
21. S9104BTE