Similarly shaped airfoils to SB98 VS5 tip
New! Bulk download of polars in Excel format: SB98%20VS5%20tip.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 CY 1025 20098
3. HQ 2.0/10
4. NACA64-410
5. NACA63A310
6. EM CY 1021 2010 X5 Fertig
7. NACA63-410
8. SB99blkm mid
9. NACA64-310 a=0.8
10. NACA64A310
11. RAF 28
12. EPPLER 224
13. EM J8 2010 DrW
14. EM J18 2010
15. NACA64-310 a=0.6
16. NACA65-410
17. NACA63-310 a=0.8
18. TP210-10%
19. SB95 9.5/2
20. NACA2410
21. HQ 2.1/9.5