Similarly shaped airfoils to NACA35118


New! Bulk download of polars in Excel format: NACA35118.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. Horten 18.00% thick 4.00% camber
2. NACA35119
3. NACA35117
4. Horten 18.00% thick 5.00% camber
5. NACA44018
6. NACA34118
7. NACA44118
8. Horten 19.00% thick 4.00% camber
9. Horten 17.00% thick 4.00% camber
10. Horten 19.00% thick 5.00% camber
11. NACA45119
12. NACA45018
13. NACA35018
14. NACA44117
15. NACA34117
16. NACA35116.5
17. NACA45118
18. Horten 17.00% thick 5.00% camber
19. NACA45019
20. NACA44017
21. NACA34119