Similarly shaped airfoils to Joukowsky 12.00% thick 2.00% camber


Direct link: Joukowsky 12.00% thick 2.00% camber
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
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 11.00% thick 2.00% camber
2. Joukowsky 13.00% thick 2.00% camber
3. OAF117
4. NM19 root
5. SB98 VR5 root
6. HN-1069b
7. EM 925 20103 181 n
8. HN-980
9. TP210-11%
10. SB95 11.5/2
11. HN-474
12. HN-1091b
13. HN-951
14. HN-1069a
15. HN-309
16. HN-1091a
17. RG 15A-1.8/11.0
18. NACA63-312 a=0.8
19. EM S5 1811 121
20. NACA63-412
21. EM S104 20107