AIR 100-2 Acro MM 576 1999


New! Bulk download of polars in Excel format: AIR%20100-2%20Acro%20MM%20576%201999.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
5AIR 100-2 Acro MM 576 1999FLAP5C40
15AIR 100-2 Acro MM 576 1999FLAP15C40
25AIR 100-2 Acro MM 576 1999FLAP25C40
35AIR 100-2 Acro MM 576 1999FLAP35C40
45AIR 100-2 Acro MM 576 1999FLAP45C40
-5AIR 100-2 Acro MM 576 1999FLAPM5C40
-15AIR 100-2 Acro MM 576 1999FLAPM15C40
-25AIR 100-2 Acro MM 576 1999FLAPM25C40
-35AIR 100-2 Acro MM 576 1999FLAPM35C40
-45AIR 100-2 Acro MM 576 1999FLAPM45C40