Similarly shaped airfoils to NACA M7 (NACA-TR-221)


New! Bulk download of polars in Excel format: NACA%20M7%20%28NACA-TR-221%29.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 M16
3. NACA M7
4. NACA M13
5. GOE 590
6. NACA45007
7. NACA M13 (NACA-TR-221)
8. GOE 393
9. GOE 122 (MVA H.2)
10. GOE 377
11. GOE 346 (FRIEDRICHSHAFEN-STAAKEN)
12. GOE 101
13. GOE 142 (MVA H.19)
14. GOE 374
15. USA 5
16. GOE 419
17. NACA45005
18. NACA45107
19. GOE 375
20. GOE 399
21. GOE 235