Similarly shaped airfoils to NACA34118
New! Bulk download of polars in Excel format: NACA34118.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. Horten 18.00% thick 4.00% camber
3. NACA34119
4. NACA34117
5. NACA34018
6. Horten 18.00% thick 3.00% camber
7. Horten 19.00% thick 4.00% camber
8. NACA35118
9. NACA44117
10. NACA44019
11. NACA44119
12. Horten 17.00% thick 4.00% camber
13. NACA35018
14. NACA44018
15. Horten 19.00% thick 3.00% camber
16. NACA34019
17. NACA35119
18. NACA25118
19. NACA34116.5
20. NACA34017
21. NACA33117