Similarly shaped airfoils to SIKORSKY SC1095
New! Bulk download of polars in Excel format: sc1095.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
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2. Horten 10.00% thick 1.00% camber
3. NACA1410
4. EPPLER 226
5. RS001m05
6. TP28-4
7. RS001m60
8. BOEING VERTOL V(1.95)3009-1.25
9. NACA1409
10. Horten 9.00% thick 1.00% camber
11. HQ 1.0/10
12. HN-961SA
13. NACA22010
14. EH 1.0/9.0
15. NACA63-110 a=0.5
16. NACA63-110 a=0.6
17. NACA22009
18. NACA63A110
19. GIII BL86
20. RS006m75
21. NACA63-210 a=0.0