Similarly shaped airfoils to Joukowsky 20.00% thick 5.00% camber


New! Bulk download of polars in Excel format: Joukowsky%2020.00%25%20thick%205.00%25%20camber.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. Joukowsky 19.00% thick 5.00% camber
2. GOE 646
3. EPPLER 748
4. Joukowsky 20.00% thick 6.00% camber
5. Joukowsky 18.00% thick 5.00% camber
6. Joukowsky 20.00% thick 4.00% camber
7. Joukowsky 19.00% thick 4.00% camber
8. GOE 420
9. Joukowsky 19.00% thick 6.00% camber
10. GOE 433
11. NACA63-720 a=0.8
12. NACA63-719 a=0.8
13. Joukowsky 18.00% thick 4.00% camber
14. GOE 679
15. Joukowsky 18.00% thick 6.00% camber
16. NACA63-720 a=0.6
17. NACA63-719 a=0.6
18. GOE 255 (MVA CA.6)
19. EPPLER 857
20. EPPLER 856
21. Joukowsky 17.00% thick 5.00% camber