Similarly shaped airfoils to NACA M16
New! Bulk download of polars in Excel format: m16.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. NACA M13
3. NACA45007
4. NACA35007
5. GOE 393
6. GOE 235
7. GOE 419
8. GOE 346 (FRIEDRICHSHAFEN-STAAKEN)
9. NACA M7
10. GOE 377
11. NACA35107
12. NACA44007
13. GOE 142 (MVA H.19)
14. GOE 101
15. NACA45005
16. GOE 122 (MVA H.2)
17. I.S.A. 571
18. GOE 100 (SOPWITH)
19. GOE 147 (MVA H.6)
20. GOE 113
21. GOE 368