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 1999FLAP5C35
15AIR 100-2 Acro MM 576 1999FLAP15C35
25AIR 100-2 Acro MM 576 1999FLAP25C35
35AIR 100-2 Acro MM 576 1999FLAP35C35
45AIR 100-2 Acro MM 576 1999FLAP45C35
-5AIR 100-2 Acro MM 576 1999FLAPM5C35
-15AIR 100-2 Acro MM 576 1999FLAPM15C35
-25AIR 100-2 Acro MM 576 1999FLAPM25C35
-35AIR 100-2 Acro MM 576 1999FLAPM35C35
-45AIR 100-2 Acro MM 576 1999FLAPM45C35