Similarly shaped airfoils to GOE 434
New! Bulk download of polars in Excel format: goe434.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 522
3. EPPLER 858
4. GOE 386
5. Joukowsky 20.00% thick 6.00% camber
6. GOE 435
7. Joukowsky 20.00% thick 5.00% camber
8. EPPLER 857
9. GA 30-620
10. GOE 383
11. GA 30A620
12. NACA6720
13. DEFIANT CANARD BL20
14. Joukowsky 19.00% thick 5.00% camber
15. Joukowsky 19.00% thick 6.00% camber
16. Joukowsky 20.00% thick 7.00% camber
17. GOE 798
18. NACA6719
19. GA 30-619
20. EPPLER 748
21. NACA63-720 a=0.8