Similarly shaped airfoils to Sipkill 1.7/10
New! Bulk download of polars in Excel format: Sipkill.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. NACA24010
3. TsAGI B 10.0% thick
4. TsAGI B 9.5% thick
5. ZAGI 10
6. FX 69-H-098
7. EH 2.0/10
8. RC-10(N)1
9. NACA2210
10. NACA25010.5
11. NACA24010.5
12. NACA23010
13. BOEING 737 MIDSPAN
14. AZcombat1
15. Horten 10.00% thick 2.00% camber
16. NACA63-310 a=0.0
17. NACA64-310 a=0.0
18. NACA2310
19. BOEING-VERTOL V23010-1.58
20. RG 14 10%
21. MH 44 9.66%