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

     Inputs:
                horsepower: 680
                     pitch: variable
            max engine rpm: 2700
        prop diameter (ft): 8

     Outputs:
              max prop rpm:2345.38
                gear ratio:   1.15
                       Cp0:0.080358
                       Ct0:0.069107
       static thrust (lbs):1028.53
-->

<propeller name="prop">
  <ixx> 7.9504 </ixx>
  <diameter unit="IN"> 96.0 </diameter>
  <numblades> 4 </numblades>
  <gearratio>1.15 </gearratio>
  <minpitch> 12 </minpitch>
  <maxpitch> 30 </maxpitch>
  <minrpm>   1994 </minrpm>
  <maxrpm>   2345 </maxrpm>

  <table name="C_THRUST" type="internal">
      <tableData>
                12         30
       0.0      0.0691   0.1091
       0.1      0.0634   0.1091
       0.2      0.0576   0.1091
       0.3      0.0478   0.1086
       0.4      0.0364   0.1080
       0.5      0.0248   0.1066
       0.6      0.0106   0.1009
       0.7      -0.0009   0.0908
       0.8      -0.0204   0.0805
       1.0      -0.0443   0.0536
       1.2      -0.0726   0.0286
       1.4      -0.0992   0.0021
       1.6      -0.1299   -0.0235
       1.8      -0.1589   -0.0489
       2.0      -0.1866   -0.0755
       2.2      -0.2142   -0.1026
       2.4      -0.2419   -0.1298
      </tableData>
  </table>

  <table name="C_POWER" type="internal">
     <tableData>
                12         30
       0.0      0.0804   0.1404
       0.1      0.0804   0.1404
       0.2      0.0766   0.1404
       0.3      0.0728   0.1404
       0.4      0.0640   0.1404
       0.5      0.0527   0.1388
       0.6      0.0427   0.1373
       0.7      0.0252   0.1342
       0.8      0.0100   0.1279
       1.0      -0.0301   0.1044
       1.2      -0.0878   0.0702
       1.4      -0.1631   0.0351
       1.6      -0.2411   -0.0031
       1.8      -0.3214   -0.0856
       2.0      -0.4018   -0.1712
       2.2      -0.4821   -0.2569
       2.4      -0.5625   -0.3425
     </tableData>
  </table>

</propeller>


