Similarly shaped airfoils to Joukowsky 9.00% thick 4.00% camber


New! Bulk download of polars in Excel format: Joukowsky%209.00%25%20thick%204.00%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. HOBIE
2. OAF095
3. Joukowsky 10.00% thick 4.00% camber
4. HOBIE SM
5. MID 107
6. MID 108a
7. FX 60-100
8. AH 79-100 A
9. SD7043 (9.1%)
10. NACA63-609 a=0.8
11. FX 60-100 (126)
12. NACA63-709
13. FX 60-100 10.0% smoothed
14. SB99 F3J
15. SB98F3J 8/3.5
16. AMI 43
17. GOE 602 MOD.
18. EM J18 3510 26 51
19. NACA64-609 a=0.8
20. MH 38 9.68%
21. HQ 3.5/9