Similarly shaped airfoils to GOE 462


New! Bulk download of polars in Excel format: goe462.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 464
2. RAF 19
3. BE6699 (6.6% max t/c 9.9% max camber) CLmax 2.1 at RE 100000 transition free
4. Joukowsky 9.00% thick 10.00% camber
5. Joukowsky 10.00% thick 10.00% camber
6. FX 74-Cl5-140 MOD (smoothed)
7. Joukowsky 11.00% thick 10.00% camber
8. GOE 481
9. EPPLER 377
10. EPPLER 377MOD
11. EPPLER 423
12. Joukowsky 9.00% thick 9.00% camber
13. SARATOV
14. EPPLER 420
15. S1223
16. Joukowsky 12.00% thick 10.00% camber
17. FX 74_CL5_140
18. EPPLER 376
19. Joukowsky 10.00% thick 9.00% camber
20. GOE 448
21. Jedeslsky EJ85