Similarly shaped airfoils to GOE 646
New! Bulk download of polars in Excel format: goe646.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 856
3. Joukowsky 19.00% thick 5.00% camber
4. GOE 255 (MVA CA.6)
5. EPPLER 748
6. GOE 679
7. Joukowsky 18.00% thick 5.00% camber
8. Joukowsky 20.00% thick 5.00% camber
9. GA 30-618
10. GA 30U-618
11. NACA63-719 a=0.8
12. GOE 433
13. NACA63-718 a=0.8
14. GA 30A618
15. GA 30-617
16. SB99A22CO
17. GOE 681
18. GA 30A617
19. NACA63A718
20. FX 84-W-175
21. Joukowsky 19.00% thick 4.00% camber