Similarly shaped airfoils to GOE 650
New! Bulk download of polars in Excel format: goe650.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. MS535-2
3. GOE 550
4. GS-1
5. GOE 430
6. NM Retro 13
7. GOE 619
8. GOE 685
9. Joukowsky 14.00% thick 5.00% camber
10. USA 40
11. EPPLER 210
12. Joukowsky 14.00% thick 4.00% camber
13. EPPLER 562
14. NACA4512-63
15. Joukowsky 13.00% thick 5.00% camber
16. Joukowsky 13.00% thick 4.00% camber
17. Joukowsky 15.00% thick 5.00% camber
18. NACA63-714 a=0.8
19. MID 403
20. NACA63-713 a=0.8
21. Joukowsky 15.00% thick 4.00% camber