MH 61

Low moment coefficient airfoil for tailless model aircraft.
See also MH 60, MH 62, MH 64.

Characteristics

Calculated Polars (PROFIL/Eppler):

Calculated Polars (X-Foil/Drela):

All Polars in XML format

Coordinates in XML format

  x        y
1.00000  0.00000
0.99662 -0.00021
0.98634 -0.00059
0.96923 -0.00048
0.94584  0.00055
0.91671  0.00267
0.88248  0.00606
0.84394  0.01072
0.80189  0.01650
0.75708  0.02313
0.71024  0.03031
0.66204  0.03762
0.61302  0.04455
0.56351  0.05077
0.51386  0.05605
0.46445  0.06025
0.41565  0.06329
0.36787  0.06513
0.32154  0.06577
0.27709  0.06518
0.23491  0.06336
0.19534  0.06033
0.15870  0.05614
0.12523  0.05090
0.09521  0.04481
0.06892  0.03804
0.04659  0.03077
0.02843  0.02321
0.01457  0.01560
0.00514  0.00829
0.00031  0.00184
0.00000  0.00000
0.00134 -0.00348
0.00856 -0.00857
0.02097 -0.01389
0.03826 -0.01907
0.06019 -0.02391
0.08653 -0.02818
0.11707 -0.03174
0.15158 -0.03446
0.18982 -0.03631
0.23147 -0.03729
0.27618 -0.03741
0.32357 -0.03676
0.37317 -0.03545
0.42447 -0.03361
0.47691 -0.03137
0.52987 -0.02886
0.58271 -0.02619
0.63480 -0.02345
0.68549 -0.02070
0.73417 -0.01799
0.78024 -0.01537
0.82314 -0.01288
0.86235 -0.01055
0.89737 -0.00841
0.92776 -0.00646
0.95315 -0.00469
0.97321 -0.00310
0.98777 -0.00161
0.99683 -0.00044
1.00000  0.00000
This airfoil has originally been published in [1].

Last modification of this page: 21.05.18

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