Similarly shaped airfoils to Joukowsky 16.00% thick 0.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2016.00%25%20thick%200.00%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. EPPLER 478
3. EPPLER 479
4. SU-26M
5. Joukowsky 15.00% thick 0.00% camber
6. Joukowsky 17.00% thick 0.00% camber
7. EPPLER 473
8. FX 71-L-150/20
9. FX 71-L-150/30
10. Horten 15.00% thick 0.00% camber
11. EPPLER 475
12. FX 71-L-150/25
13. EPPLER 169
14. EPPLER 477
15. Joukowsky 14.00% thick 0.00% camber
16. Joukowsky 18.00% thick 0.00% camber
17. Joukowsky 16.00% thick 1.00% camber
18. EPPLER 474
19. Horten 16.00% thick 0.00% camber
20. GA 35-016
21. GA 30-015