Similarly shaped airfoils to Joukowsky 9.00% thick 3.00% camber


New! Bulk download of polars in Excel format: Joukowsky%209.00%25%20thick%203.00%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. MID 108b
2. S2046
3. Joukowsky 10.00% thick 3.00% camber
4. AG3516
5. MID 29
6. S4110
7. GOE 565
8. EPPLER 64
9. HN-424
10. avx-planeur
11. HN-354OC
12. HN-418
13. JWL043 8.8/2.1
14. JWL042 8.6/2.5
15. SD7037-092-88
16. HS 602
17. MID 108a
18. HN-839D
19. NACA63-509
20. JWL046 9.2/2.6
21. JWL045 9.2/2.7