<?xml version="1.0"?>
<!--
  Converted from a file generated by Aero-Matic v 0.7
-->

<propeller name="prop">
  <ixx> 3.79106 </ixx>
  <diameter unit="IN"> 165.0 </diameter>
  <numblades> 4 </numblades>
  <minpitch> 10.0 </minpitch>
  <maxpitch> 30.0 </maxpitch>
  <minrpm>    700 </minrpm>
  <maxrpm>   1400 </maxrpm>

  <table name="C_THRUST" type="internal">
    <tableData>
           10      30
      0.0  0.07488 0.0936
      0.1  0.07416 0.0927
      0.2  0.07344 0.0918
      0.3  0.07272 0.0909
      0.4  0.06625 0.0828
      0.5  0.05904 0.0738
      0.6  0.05040 0.0630
      0.7  0.03920 0.0490
      0.8  0.02880 0.0360
      0.9  0.01600 0.0200
      1.0  0.00320 0.0040
    </tableData>
  </table>

  <table name="C_POWER" type="internal">
    <tableData>
           10      30
      0.0  0.02287 0.10395
      0.1  0.02252 0.10237
      0.2  0.02217 0.10080
      0.3  0.02148 0.09765
      0.4  0.02079 0.09450
      0.5  0.02009 0.09135
      0.6  0.01905 0.08662
      0.7  0.01663 0.07560
      0.8  0.01316 0.05985
      0.9  0.00866 0.03937
      1.0  0.00346 0.01575
    </tableData>
  </table>

</propeller>
