Similarly shaped airfoils to Joukowsky 19.00% thick 8.00% camber


Direct link: Joukowsky 19.00% thick 8.00% 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 18.00% thick 8.00% camber
2. Joukowsky 20.00% thick 8.00% camber
3. Joukowsky 19.00% thick 9.00% camber
4. Joukowsky 17.00% thick 8.00% camber
5. GOE 222 (MVA H.33)
6. Joukowsky 19.00% thick 7.00% camber
7. Joukowsky 20.00% thick 9.00% camber
8. Joukowsky 18.00% thick 7.00% camber
9. GOE 228 (MVA H.38)
10. Joukowsky 18.00% thick 9.00% camber
11. Joukowsky 20.00% thick 7.00% camber
12. Joukowsky 17.00% thick 7.00% camber
13. Joukowsky 17.00% thick 9.00% camber
14. MH 112 16.2%
15. Joukowsky 16.00% thick 8.00% camber
16. GOE 217 (MVA MK.12)
17. GOE 243 (MVA PR.3)
18. Joukowsky 16.00% thick 7.00% camber
19. GOE 241 (MVA PR.1)
20. GOE 441
21. GOE 421