Similarly shaped airfoils to NACA34016.5


New! Bulk download of polars in Excel format: NACA34016.5.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. NACA34017
2. NACA34016
3. Horten 17.00% thick 3.00% camber
4. NACA25116.5
5. NACA33016.5
6. Horten 16.00% thick 3.00% camber
7. NACA33016
8. NACA25116
9. NACA25117
10. NACA33017
11. NACA34116.5
12. NACA34116
13. GA(PC)1 climb flap
14. NACA34117
15. NACA33116.5
16. NACA44016.5
17. NACA33116
18. NACA44017
19. Horten 17.00% thick 2.00% camber
20. Horten 16.00% thick 2.00% camber
21. Horten 17.00% thick 4.00% camber