Similarly shaped airfoils to Joukowsky 13.00% thick 0.00% camber


New! Bulk download of polars in Excel format: Joukowsky%2013.00%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. HM50T
2. EPPLER 168
3. Joukowsky 12.00% thick 0.00% camber
4. Joukowsky 14.00% thick 0.00% camber
5. FX 71-120
6. EPPLER 169
7. FX 79-L-120
8. GOE 429
9. EPPLER 472
10. Horten 12.00% thick 0.00% camber
11. EPPLER EA 6(-1)-012
12. FX LIII-142 K 25
13. FX 76-120
14. BOEING 737 MIDSPAN
15. GA 30-012
16. Horten 13.00% thick 0.00% camber
17. GA 35-013
18. NACA0012
19. HN-976S
20. EPPLER 171
21. GA 35-012