Similarly shaped airfoils to NACA45013
New! Bulk download of polars in Excel format: NACA45013.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. EPPLER 338
3. ONERA OA213
4. NACA45014
5. NACA45012
6. EPPLER 329
7. NACA44012
8. NACA35013
9. HS 3.4.12b
10. NACA35113
11. HS 3.5/12
12. NACA35013.5
13. HL80-133
14. NACA35113.5
15. NACA45014.5
16. NACA44013
17. EPPLER 637
18. EPPLER 334
19. NACA63-613 a=0.0
20. NACA63-614 a=0.0
21. BOEING VERTOL V43012-1.58