Similarly shaped airfoils to Joukowsky 17.00% thick 0.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2017.00%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. GOE 410
3. Joukowsky 16.00% thick 0.00% camber
4. Joukowsky 18.00% thick 0.00% camber
5. SU-26M
6. EPPLER 478
7. EPPLER 473
8. Horten 16.00% thick 0.00% camber
9. Joukowsky 17.00% thick 1.00% camber
10. Joukowsky 15.00% thick 0.00% camber
11. Joukowsky 19.00% thick 0.00% camber
12. Horten 15.00% thick 0.00% camber
13. GA 35-017
14. Horten 17.00% thick 0.00% camber
15. GA 30-016
16. EPPLER 475
17. Horten 16.00% thick 1.00% camber
18. GA 35-016
19. NACA0016
20. TRAINER60
21. Joukowsky 18.00% thick 1.00% camber