Similarly shaped airfoils to Joukowsky 14.00% thick 8.00% camber


New! Bulk download of polars in Excel format: Joukowsky%2014.00%25%20thick%208.00%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 227 (MVA H.37)
2. Joukowsky 15.00% thick 8.00% camber
3. Joukowsky 13.00% thick 8.00% camber
4. GOE 226 (MVA H.36)
5. GOE 225 (MVA H.35)
6. Joukowsky 12.00% thick 8.00% camber
7. Joukowsky 16.00% thick 8.00% camber
8. Joukowsky 14.00% thick 7.00% camber
9. Joukowsky 14.00% thick 9.00% camber
10. Joukowsky 13.00% thick 7.00% camber
11. FX 73-CL3-152
12. Joukowsky 15.00% thick 9.00% camber
13. GOE 242 (MVA PR.2)
14. Joukowsky 15.00% thick 7.00% camber
15. FX 73-CL2-152
16. Joukowsky 13.00% thick 9.00% camber
17. FX 76-MP-120
18. MH 113 14.62%
19. FX 72-MS-150A
20. GOE 441
21. EPPLER 591