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
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 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