<?xml version="1.0"?>

<propeller name="Fixed-Pitch 75-inch Two-Blade Propeller">
  <ixx> 1.67 </ixx>
  <diameter unit="IN"> 75.0 </diameter>
  <numblades> 2 </numblades>
  <minpitch> 22 </minpitch>
  <maxpitch> 22 </maxpitch>

  <!--table name="C_THRUST" type="internal">
    <tableData>
      0.0   0.068
      0.1   0.068
      0.2   0.067
      0.3   0.066
      0.4   0.064
      0.5   0.061
      0.6   0.057
      0.7   0.050
      0.8   0.040
      0.9   0.029
      1.0   0.019
      1.1   0.008
      1.2   -0.001
      1.3   -0.008
      1.4   -0.019
      1.5   -0.029
      1.6   -0.040
      1.7   -0.050
      1.8   -0.057
      1.9   -0.061
      2.0   -0.064
      2.1   -0.066
      2.2   -0.067
      2.3   -0.068
      5.0   -0.068
    </tableData>
  </table-->

  <table name="C_THRUST" type="internal">
    <tableData>
      0.0   0.073
      0.1   0.073
      0.2   0.072
      0.3   0.071
      0.4   0.069
      0.5   0.066
      0.6   0.062
      0.7   0.055
      0.8   0.045
      0.9   0.034
      1.0   0.024
      1.1   0.013
      1.2   -0.006
      1.3   -0.013
      1.4   -0.024
      1.5   -0.034
      1.6   -0.045
      1.7   -0.055
      1.8   -0.062
      1.9   -0.066
      2.0   -0.069
      2.1   -0.071
      2.2   -0.072
      2.3   -0.073
      5.0   -0.073
    </tableData>
  </table>

  <!--table name="C_POWER" type = "internal">
    <tableData>
      0.0   0.0580
      0.1   0.0620
      0.2   0.0600
      0.3   0.0580
      0.4   0.0520
      0.5   0.0450
      0.6   0.0421
      0.7   0.0389
      0.8   0.0346
      0.9   0.0280
      1.0   0.0202
      1.1   0.0111
      1.2   0.0075
      1.3   0.0111
      1.4   0.0202
      1.5   0.0280
      1.6   0.0346
      1.7   0.0389
      1.8   0.0421
      1.9   0.0436
      2.0   0.0445
      2.1   0.0445
      2.2   0.0442
      2.3   0.0431
      2.4   0.0424
      5.0   0.0413
    </tableData>
  </table-->

  <table name="C_POWER" type = "internal">
    <tableData>
      0.0   0.0660
      0.1   0.0700
      0.2   0.0700
      0.3   0.0660
      0.4   0.0600
      0.5   0.0530
      0.6   0.0501
      0.7   0.0469
      0.8   0.0426
      0.9   0.0360
      1.0   0.0282
      1.1   0.0191
      1.2   0.0155
      1.3   0.0191
      1.4   0.0282
      1.5   0.0360
      1.6   0.0426
      1.7   0.0469
      1.8   0.0501
      1.9   0.0516
      2.0   0.0525
      2.1   0.0525
      2.2   0.0522
      2.3   0.0511
      2.4   0.0504
      5.0   0.0493
    </tableData>
  </table>

<!-- thrust effects of helical tip Mach -->
<table name="CT_MACH" type="internal">
  <tableData>
    0.85   1.0
    1.05   0.8
  </tableData>
</table>

<!-- power-required effects of helical tip Mach -->
<table name="CP_MACH" type="internal">
  <tableData>
    0.85   1.0
    1.05   1.8
    2.00   1.4
  </tableData>
</table>

</propeller>
