Similarly shaped airfoils to Joukowsky 10.00% thick 3.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2010.00%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
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 9.00% thick 3.00% camber
3. Joukowsky 11.00% thick 3.00% camber
4. EM J18 2610 27 48
5. EM J18 2510 26 51
6. EM J18 3010 26 51
7. S2046
8. EM L3 2510
9. MH 117 9.8%
10. FX 60-100 10.0% smoothed
11. EM J20 2510
12. SD7037-092-88
13. JWL045 9.2/2.7
14. JWL046 9.2/2.6
15. EM J19 3010
16. HN-424
17. OAF102
18. EM J8 3010 DrW
19. EM J8 2510 DrW
20. SA7036
21. SA7035