Similarly shaped airfoils to Joukowsky 12.00% thick 0.00% camber


New! Bulk download of polars in Excel format: Joukowsky%2012.00%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
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. GOE 429
2. EPPLER 168
3. HN-976S
4. Joukowsky 11.00% thick 0.00% camber
5. Joukowsky 13.00% thick 0.00% camber
6. EPPLER 428
7. EPPLER 472
8. FX 79-L-120
9. HN-478S
10. Horten 11.00% thick 0.00% camber
11. EPPLER 426
12. HM50T
13. JWL069 11/0
14. FX 71-120
15. HN-477S
16. GA 30-011
17. Horten 12.00% thick 0.00% camber
18. GA 35-012
19. HN-275S
20. NACA63-012
21. GA 35-011