Similarly shaped airfoils to NACA44112
New! Bulk download of polars in Excel format: NACA44112.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. NACA44113
3. Horten 12.00% thick 4.00% camber
4. NACA35112
5. NACA34113
6. Horten 13.00% thick 4.00% camber
7. NACA35113
8. EPPLER 636
9. Horten 11.00% thick 4.00% camber
10. Horten 12.00% thick 5.00% camber
11. NACA44113.5
12. HS 3.5/12
13. NACA44013
14. NACA44012
15. NACA45113
16. NACA34110.5
17. Horten 13.00% thick 5.00% camber
18. HS 3.4.12b
19. EPPLER 332
20. EPPLER 637
21. NACA35113.5