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
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

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

1. NACA M16 (NACA-TR-221)
2. NACA M13 (NACA-TR-221)
3. GOE 590
4. NACA M13
5. NACA M7 (NACA-TR-221)
6. NACA45007
7. NACA35007
8. GOE 393
9. GOE 235
10. GOE 419
11. GOE 346 (FRIEDRICHSHAFEN-STAAKEN)
12. NACA M7
13. GOE 377
14. NACA35107
15. NACA44007
16. GOE 142 (MVA H.19)
17. GOE 101
18. NACA45005
19. GOE 122 (MVA H.2)
20. I.S.A. 571
21. GOE 100 (SOPWITH)