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

     Inputs:
                horsepower: 85.5
                     pitch: fixed
            max engine rpm: 1350
        prop diameter (ft): 9

     Outputs:
              max prop rpm:2084.78
                gear ratio:   0.65
                       Cp0:0.007983
                       Ct0:0.006866
       static thrust (lbs): 129.32
-->
<!--
   From [AHT,
   http://www.aht.ndirect.co.uk/airships/Technical%20Spec/SSZ%20Airship.htm]:

    Propeller               Four-bladed 9 feet diameter
-->
<propeller name="prop">
  <ixx> 5.6600 </ixx>
  <diameter unit="IN">108.0 </diameter>
  <numblades> 4 </numblades>
  <gearratio>1.0</gearratio>

  <table name="C_THRUST" type="internal">
     <tableData>
   0.00000   0.02622
   0.10000   0.02508
   0.20000   0.02394
   0.30000   0.02204
   0.40000   0.01976
   0.50000   0.01748
   0.60000   0.01406
   0.70000   0.01064
   0.80000   0.00570
   1.00000  -0.00190
   1.20000  -0.01026
   1.40000  -0.01862
     </tableData>
  </table>

  <table name="C_POWER" type="internal">
     <tableData>
   0.00000   0.02400
   0.10000   0.02400
   0.20000   0.02340
   0.30000   0.02280
   0.40000   0.02160
   0.50000   0.01980
   0.60000   0.01800
   0.70000   0.01530
   0.80000   0.01230
   1.00000   0.00450
   1.20000  -0.00720
   1.40000  -0.02130
     </tableData>
  </table>

</propeller>
