Similarly shaped airfoils to GA 40-016
New! Bulk download of polars in Excel format: GA%2040-016.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 37A016
3. EPPLER 837 HYDROFOIL
4. LWK 80-150/K25
5. NACA63A016
6. GA 35A016
7. NACA65-116 a=0.0
8. NACA65-116
9. GA 37-016
10. NACA65-116 a=0.2
11. NACA65-015
12. GA 40A015
13. GA 40-015
14. GA 40-017
15. GA 40A017
16. NACA64(2)-015A
17. GA 37A015
18. NACA65-116 a=0.8
19. NACA65-116 a=0.5
20. NACA63A015
21. GA 37-017