Similarly shaped airfoils to LWK 80-150/K25
New! Bulk download of polars in Excel format: lwk80150k25.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. GA 40A016
3. GA 37A016
4. GA 40A015
5. GA 37A015
6. NACA64(2)-015A
7. NACA65-015
8. GA 40-015
9. GA 35A016
10. NACA63A015
11. NACA63A016
12. GA 35A015
13. NACA63-015A
14. NACA66-015
15. EPPLER 837 HYDROFOIL
16. NACA65-116 a=0.0
17. NACA65-116
18. NACA65-116 a=0.2
19. GA 37-016
20. NACA65-115 a=0.0
21. NACA65-115