jsbsim.js/JSBSim/engine/Dr1_propeller.xml

JSBSim flight dynamics model ported to JavaScript

<?xml version="1.0"?>
<!-- Generated by javaprop

     Inputs:
          Number of Blades:  2
                       rpm: 1200
         prop diameter (M): 2.59
      spinner diameter (M): 0.222
            velocity (m/s): 60.0
                     power: 66 kWatts
                  Airfoils: Clark Y, Re 1e5

       static thrust (lbs): 340
-->

<propeller name="prop">
  <ixx> 14.7913 </ixx>         <!-- aeromatic: 4.7681, selig engine: 10.0232 -->
  <diameter unit="IN">102.0 </diameter>
  <numblades> 2 </numblades>
  <gearratio>1.0 </gearratio>

  <table name="C_THRUST" type="internal">
     <tableData>
0.00	0.068859
0.10	0.073298
0.20	0.073756
0.30	0.072814
0.40	0.071237
0.50	0.069318
0.60	0.067693
0.70	0.067243
0.80	0.067742
0.90	0.065086
1.00	0.060402
1.10	0.050696
1.20	0.038775
1.30	0.026630
1.32	0.024174
1.34	0.021711
1.36	0.019236
1.38	0.016754
1.40	0.014264
1.42	0.011765
1.44	0.009257
1.46	0.006727
1.48	0.004182
1.50	0.001634
1.52	-0.000919
     </tableData>
  </table>


  <table name="C_POWER" type="internal">
     <tableData>
0.00	0.074862
0.10	0.084784
0.20	0.081415
0.30	0.079246
0.40	0.076760
0.50	0.074810
0.60	0.073155
0.70	0.072521
0.80	0.072807
0.90	0.072948
1.00	0.071388
1.10	0.064260
1.20	0.053052
1.30	0.039761
1.32	0.036846
1.34	0.033848
1.36	0.030759
1.38	0.027584
1.40	0.024322
1.42	0.020971
1.44	0.017532
1.46	0.013984
1.48	0.010335
1.50	0.006603
1.52	0.002785
     </tableData>
  </table>

</propeller>