Similarly shaped airfoils to NACA34018
New! Bulk download of polars in Excel format: NACA34018.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 3.00% camber
3. NACA25118
4. NACA33018
5. NACA34019
6. NACA34017
7. NACA34118
8. NACA35019
9. NACA44019
10. Horten 19.00% thick 3.00% camber
11. Horten 18.00% thick 2.00% camber
12. NACA44018
13. NACA33017
14. NACA25117
15. Horten 17.00% thick 3.00% camber
16. Horten 18.00% thick 4.00% camber
17. NACA24118
18. NACA25119
19. NACA25018
20. NACA34117
21. NACA33117