Similarly shaped airfoils to Joukowsky 19.00% thick 5.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2019.00%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
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. Joukowsky 20.00% thick 5.00% camber
3. GOE 646
4. GOE 433
5. EPPLER 748
6. Joukowsky 19.00% thick 6.00% camber
7. Joukowsky 17.00% thick 5.00% camber
8. Joukowsky 19.00% thick 4.00% camber
9. Joukowsky 20.00% thick 6.00% camber
10. GOE 420
11. Joukowsky 18.00% thick 4.00% camber
12. Joukowsky 18.00% thick 6.00% camber
13. Joukowsky 20.00% thick 4.00% camber
14. EPPLER 856
15. EPPLER 1211
16. GOE 413
17. NACA63-719 a=0.8
18. NACA63-718 a=0.8
19. EPPLER 561
20. GOE 288
21. Joukowsky 17.00% thick 4.00% camber