Similarly shaped airfoils to MS2-9,5
New! Bulk download of polars in Excel format: MS2-9%2C5.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. SB95 9.5/2
3. SB97EP 9.2/1.9
4. S6061 9%
5. FAD13
6. NM18 root
7. FAD14
8. NM19-S tip
9. MS1,9-8,7
10. HN-350M01
11. NACA2409
12. HQ 2.0/9
13. SB99blkm mid
14. NACA63-310 a=0.5
15. HQ-2.0/9 9.0% smoothed
16. SB99blkr root
17. NACA63-310 a=0.6
18. NM18-S tip
19. SB99blks tip
20. HS 1.7/9
21. HQ 2.1/9.5