Similarly shaped airfoils to NACA44121
New! Bulk download of polars in Excel format: NACA44121.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. NACA44021
3. NACA34121
4. NACA45121
5. Horten 20.00% thick 5.00% camber
6. Horten 20.00% thick 4.00% camber
7. NACA34021
8. NACA44119
9. NACA35021
10. NACA25121
11. Horten 20.00% thick 3.00% camber
12. NACA34119
13. Horten 19.00% thick 4.00% camber
14. NACA44019
15. NACA45021
16. NACA35119
17. NACA33121
18. NACA45119
19. Horten 20.00% thick 6.00% camber
20. NACA34019
21. NACA33021