Similarly shaped airfoils to NACA45107
New! Bulk download of polars in Excel format: NACA45107.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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2. NACA35107
3. NACA45007
4. NACA44107
5. NACA M7 (NACA-TR-221)
6. NACA45105
7. NACA44007
8. NACA45109
9. Horten 9.00% thick 6.00% camber
10. NACA M16
11. NACA M16 (NACA-TR-221)
12. NACA 11-H-09
13. Horten 9.00% thick 5.00% camber
14. NACA44105
15. NACA35105
16. NACA M17
17. GOE 746
18. NACA M17 (NACA-TR-221)
19. GOE 315 (HANSA-BRANDENBURG III.5)
20. NACA34107
21. NACA35007