Similarly shaped airfoils to Joukowsky 11.00% thick 2.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2011.00%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. Joukowsky 10.00% thick 2.00% camber
3. NM19 root
4. Joukowsky 12.00% thick 2.00% camber
5. EM J18 2010 27 48
6. EM J18 2010 26 51
7. NM18 root
8. EM 925 20103 181 n
9. NM20 root
10. NM19-S tip
11. EPPLER 224
12. HN-1069c
13. SB99blkr root
14. FAD14
15. EM J18 2010
16. EM J8 2010 DrW
17. TP210-10%
18. EM L5 2010
19. CB2195-25d
20. SB95 10.5/2
21. TPR-95-96-95