Similarly shaped airfoils to Joukowsky 9.00% thick 6.00% camber


New! Bulk download of polars in Excel format: Joukowsky%209.00%25%20thick%206.00%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. Joukowsky 10.00% thick 6.00% camber
2. GOE 500
3. EPPLER 385
4. GOE 358
5. HL73-650
6. GOE 195
7. NACA6409
8. Joukowsky 11.00% thick 6.00% camber
9. GOE 499
10. Joukowsky 9.00% thick 5.00% camber
11. Joukowsky 9.00% thick 7.00% camber
12. Eiffel 36
13. AH 79-100 B
14. GOE 176 (ALBATROS 7020)
15. GOE 610-B MOD.
16. Joukowsky 10.00% thick 7.00% camber
17. GOE 118 (MVA MK.7)
18. GOE 496
19. Joukowsky 10.00% thick 5.00% camber
20. SG6043
21. GOE 164 (MVA MK.10)