Similarly shaped airfoils to NACA45018
New! Bulk download of polars in Excel format: NACA45018.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. NACA45019
3. NACA45017
4. NACA35017
5. NACA44017
6. NACA35018
7. NACA35118
8. TsAGI B 17.5% thick
9. NACA45016.5
10. TsAGI B 18.0% thick
11. TsAGI B 17.0% thick
12. NACA35117
13. NACA35016.5
14. NACA44016.5
15. Horten 18.00% thick 5.00% camber
16. NACA45118
17. TsAGI B 18.5% thick
18. NACA35019
19. NACA35119
20. TsAGI B 16.5% thick
21. Horten 18.00% thick 4.00% camber