NACA M22 (NACA-TR-221)


New! Bulk download of polars in Excel format: NACA%20M22%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.


Angle (deg),
positive is trailing edge down
DAT File
5NACA M22 (NACA-TR-221)FLAP5C25
15NACA M22 (NACA-TR-221)FLAP15C25
25NACA M22 (NACA-TR-221)FLAP25C25
35NACA M22 (NACA-TR-221)FLAP35C25
45NACA M22 (NACA-TR-221)FLAP45C25
-5NACA M22 (NACA-TR-221)FLAPM5C25
-15NACA M22 (NACA-TR-221)FLAPM15C25
-25NACA M22 (NACA-TR-221)FLAPM25C25
-35NACA M22 (NACA-TR-221)FLAPM35C25
-45NACA M22 (NACA-TR-221)FLAPM45C25