Similarly shaped airfoils to GOE 257


New! Bulk download of polars in Excel format: goe257.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 286
2. NACA M14
3. AQUILA 9.3% smoothed
4. GOE 408
5. GOE 490
6. GOE 188
7. GOE 134 (MVA H.12)
8. GOE 316 (HANSA-BRANDENBURG IV.5)
9. GOE 328
10. GOE 596
11. GOE 277 (DAIMLER VIII)
12. GOE 385
13. GOE 309 (MVA H.41)
14. GOE 167 (V.KARMAN PROP.2)
15. NACA65-709 a=0.0
16. GOE 310 (MVA H.42)
17. NACA64-709 a=0.0
18. NACA64-709 a=0.2
19. NACA65-709 a=0.2
20. NACA63-709 a=0.0
21. GOE 180 (MVA H.26)