Similarly shaped airfoils to Joukowsky 12.00% thick 7.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2012.00%25%20thick%207.00%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
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.
2. Joukowsky 13.00% thick 7.00% camber
3. GOE 431
4. GOE 501
5. DAE-31
6. Joukowsky 10.00% thick 7.00% camber
7. Joukowsky 14.00% thick 7.00% camber
8. MID 405e
9. Joukowsky 12.00% thick 6.00% camber
10. Joukowsky 12.00% thick 8.00% camber
11. GOE 225 (MVA H.35)
12. Joukowsky 13.00% thick 8.00% camber
13. Joukowsky 11.00% thick 6.00% camber
14. AH 79-100 B
15. AH 79-100 C
16. Joukowsky 13.00% thick 6.00% camber
17. Joukowsky 11.00% thick 8.00% camber
18. MH 114 13.02%
19. DAE-21
20. GOE 239 (MVA H.31)
21. MID 405w2