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
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. 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