Similarly shaped airfoils to NACA34010.5
New! Bulk download of polars in Excel format: NACA34010.5.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
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. NACA35010.5
3. NACA35010
4. NACA33010.5
5. NACA33010
6. Horten 11.00% thick 3.00% camber
7. Horten 10.00% thick 3.00% camber
8. Phoenix10
9. NACA34110.5
10. NACA34110
11. FAD23
12. NACA25110.5
13. EPPLER 332
14. NACA44010.5
15. JWL076 10/3
16. RC(5)-10
17. BOEING-VERTOL VR-12
18. NACA33110.5
19. NACA25110
20. RC(4)-10
21. NACA33110