Similarly shaped airfoils to GOE 358
New! Bulk download of polars in Excel format: goe358.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 165 (MVA MK.11)
3. Joukowsky 11.00% thick 6.00% camber
4. Joukowsky 9.00% thick 6.00% camber
5. GOE 500
6. GOE 496
7. GOE 190 (MVA MK.18)
8. Joukowsky 10.00% thick 5.00% camber
9. GOE 176 (ALBATROS 7020)
10. Joukowsky 9.00% thick 5.00% camber
11. Joukowsky 11.00% thick 5.00% camber
12. GOE 195
13. EPPLER 216
14. Joukowsky 12.00% thick 6.00% camber
15. GOE 239 (MVA H.31)
16. EPPLER 385
17. SG6043
18. NACA6409
19. HL73-650
20. MH 115 11.06%
21. NACA6410