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
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. 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%