Similarly shaped airfoils to Joukowsky 10.00% thick 2.00% camber


New! Bulk download of polars in Excel format: Joukowsky%2010.00%25%20thick%202.00%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. CB2195-25d
2. EM J18 2010 27 48
3. EM J18 2010 26 51
4. NM18 root
5. Joukowsky 9.00% thick 2.00% camber
6. Joukowsky 11.00% thick 2.00% camber
7. NM20 root
8. NM19-S tip
9. SB97EP 9.2/1.9
10. SD5060 (9.5%)
11. SD8000-089-88
12. FAD14
13. NM18-S tip
14. RS001
15. SB99blkr root
16. FAD13
17. SB95 9.5/2
18. EM J18 2010
19. EM J8 2010 DrW
20. MS2-9,5
21. NM20-S tip