Similarly shaped airfoils to NACA45012


New! Bulk download of polars in Excel format: NACA45012.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. NACA44012
2. EPPLER 334
3. NACA45013
4. EPPLER 637
5. HS 3.4.12b
6. HS 3.5/12
7. ONERA OA213
8. USA 45 M
9. NACA35012
10. BOEING VERTOL V43012-1.58
11. NACA M15 (NACA-TR-221)
12. NACA35112
13. EPPLER 638
14. Ritz 3-30-12
15. NACA63-612 a=0.0
16. EPPLER 338
17. BOEING-VERTOL VR-7
18. NACA45013.5
19. NACA45010.5
20. NACA M18
21. NACA63-613 a=0.0