<?xml version="1.0"?>
<!-- Generated by Aero-Matic v 0.8

     Inputs:
                horsepower: 1200
                     pitch: variable
            max engine rpm: 2500
        prop diameter (ft): 11.583333333333

     Outputs:
              max prop rpm:1619.83
                gear ratio:   1.54
                       Cp0:0.067641
                       Ct0:0.058172
       static thrust (lbs):1815.06
-->

<propeller name="prop">
  <ixx>35 </ixx>
  <diameter unit="IN">139.0 </diameter>
  <numblades> 3 </numblades>
  <gearratio>1.54 </gearratio>
  <minpitch> 12 </minpitch>
  <maxpitch> 30 </maxpitch>
  <minrpm>   1400 </minrpm>
  <maxrpm>   1700 </maxrpm>
  <ct_factor> 1.20 </ct_factor>
  <cp_factor> 0.80 </cp_factor>
  <table name="C_THRUST" type="internal">
    <tableData>
              12       30
      0.0      0.0582   0.0982
      0.1      0.0533   0.0982
      0.2      0.0485   0.0982
      0.3      0.0403   0.0977
      0.4      0.0306   0.0972
      0.5      0.0209   0.0959
      0.6      0.0090   0.0908
      0.7     -0.0008   0.0817
      0.8     -0.0172   0.0725
      1.0     -0.0373   0.0482
      1.2     -0.0611   0.0257
      1.4     -0.0835   0.0019
      1.6     -0.1094  -0.0211
      1.8     -0.1338  -0.0440
      2.0     -0.1571  -0.0679
      2.2     -0.1803  -0.0923
      2.4     -0.2036  -0.1168
    </tableData>
  </table>

  <table name="C_POWER" type="internal">
    <tableData>
              12       30
      0.0      0.0676   0.1276
      0.1      0.0676   0.1276
      0.2      0.0645   0.1276
      0.3      0.0613   0.1276
      0.4      0.0539   0.1276
      0.5      0.0444   0.1262
      0.6      0.0359   0.1248
      0.7      0.0212   0.1220
      0.8      0.0085   0.1163
      1.0     -0.0254   0.0950
      1.2     -0.0739   0.0638
      1.4     -0.1373   0.0319
      1.6     -0.2029  -0.0028
      1.8     -0.2706  -0.0779
      2.0     -0.3382  -0.1557
      2.2     -0.4058  -0.2336
      2.4     -0.4735  -0.3114
    </tableData>
  </table>

</propeller>
