Similarly shaped airfoils to CB2195-25d


New! Bulk download of polars in Excel format: CB2195-25d.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. EM J18 2010 26 51
2. SB97EP 9.2/1.9
3. EM J18 2010 27 48
4. SD8000-089-88
5. NM18 root
6. Joukowsky 10.00% thick 2.00% camber
7. NM18-S tip
8. SD5060 (9.5%)
9. NM19-S tip
10. HN-350M01
11. FAD13
12. MS2-9,5
13. FAD14
14. MVR120
15. SB99blkr root
16. HN-1051
17. Joukowsky 9.00% thick 2.00% camber
18. SB95 9.5/2
19. HQ 2.0/9
20. HQ-2.0/9 9.0% smoothed
21. S7012 8.75%