Similarly shaped airfoils to LWK 80-100


New! Bulk download of polars in Excel format: lwk80100.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
Dynamic plotter New!
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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1. RAE 104
2. RAE 103
3. SC(2)-0010
4. NACA64A-010
5. GA 37A010
6. GA 40A011
7. NACA63A010
8. GA 40-011
9. GA 40A010
10. ONERA D, SHARP TRAILING EDGE
11. ONERA D, BLUNT TRAILING EDGE
12. GA 40-010
13. GA 37A011
14. GA 35A010
15. NACA0010-64
16. NACA63A011
17. GA 35A011
18. NACA0010-34
19. RAE 102
20. N-12
21. GA 37-011