jsbsim.js
Version:
JSBSim flight dynamics model ported to JavaScript
81 lines (74 loc) • 3.53 kB
text/xml
<!-- Generated by Aero-Matic v 1
Inputs:
horsepower: 1940.0
pitch: variable
max engine rpm: 3000
prop diameter (ft): 11.5
Outputs:
max prop rpm: 1631.57
gear ratio: 1.84
Cp0: 0.110944
Ct0: 0.258500
static thrust (lbs): 7950.04
-->
<propeller name="prop">
<ixx>23.6164 </ixx>
<diameter unit="IN">138.0 </diameter>
<numblades> 4 </numblades>
<gearratio>2.38</gearratio>
<minpitch>23</minpitch>
<maxpitch>65</maxpitch>
<minrpm>756</minrpm> <!-- 1800 to 3000 engine RPM -->
<maxrpm>1260</maxrpm>
<ct_factor> 1.2 </ct_factor>
<cp_factor> 0.95 </cp_factor>
<table name="C_THRUST" type="internal">
<tableData>
15 25 35 45 55 65
0.0 0.2068 0.2534 0.2792 0.2974 0.2779 0.2326
0.2 0.1696 0.2358 0.2615 0.2825 0.2640 0.2210
0.4 0.1243 0.2273 0.2498 0.2726 0.2571 0.2152
0.6 0.0622 0.1934 0.2262 0.2512 0.2398 0.2036
0.8 0.0032 0.1344 0.2038 0.2248 0.2226 0.1890
1.0 -0.0532 0.0798 0.1903 0.2076 0.2148 0.1841
1.2 -0.1094 0.0246 0.1564 0.2005 0.2148 0.1841
1.4 -0.1598 -0.0430 0.1351 0.2370 0.2530 0.2210
1.6 -0.1682 -0.1150 0.0775 0.2405 0.2612 0.2326
1.8 -0.1682 -0.1682 0.0130 0.2068 0.2534 0.2326
2.0 -0.1787 -0.1787 -0.0549 0.1716 0.2681 0.2472
2.2 -0.2522 -0.2522 -0.1746 0.1746 0.3722 0.3490
2.4 -0.2733 -0.2733 -0.2733 0.1008 0.3293 0.3780
2.6 -0.3153 -0.3153 -0.3153 0.0147 0.2405 0.3878
2.8 -0.3889 -0.3889 -0.3889 -0.1077 0.1943 0.3889
3.0 -0.4099 -0.4099 -0.4099 -0.2459 0.1074 0.3151
3.2 -0.4309 -0.4309 -0.4309 -0.3975 0.0100 0.2321
3.4 -0.4519 -0.4519 -0.4519 -0.4519 -0.0972 0.1389
3.6 -0.4730 -0.4730 -0.4519 -0.4519 -0.2051 0.0350
</tableData>
</table>
<table name="C_POWER" type="internal">
<tableData>
15 25 35 45 55 65
0.0 0.1109 0.2740 0.4848 0.7211 0.8354 0.9208
0.2 0.1073 0.2552 0.4637 0.7211 0.8354 0.9208
0.4 0.0924 0.2352 0.4404 0.7211 0.8354 0.9208
0.6 0.0610 0.2186 0.4127 0.7067 0.8321 0.9208
0.8 0.0185 0.1853 0.3883 0.6745 0.8321 0.9208
1.0 0.0185 0.1298 0.3661 0.6401 0.8288 0.9208
1.2 -0.0610 0.0499 0.3240 0.6135 0.8232 0.9208
1.4 -0.0921 -0.0369 0.2496 0.6046 0.8132 0.9208
1.6 -0.1076 -0.1109 0.1575 0.5880 0.7955 0.8876
1.8 -0.1109 -0.1853 0.0463 0.5214 0.7711 0.8687
2.0 -0.1420 -0.2585 -0.0555 0.4438 0.7344 0.8509
2.2 -0.1742 -0.3328 -0.1664 0.3606 0.7123 0.8132
2.4 -0.2052 -0.4072 -0.2774 0.2574 0.6912 0.7955
2.6 -0.2363 -0.4804 -0.3517 0.1076 0.6745 0.7677
2.8 -0.2685 -0.5547 -0.4216 -0.0366 0.6601 0.7577
3.0 -0.2995 -0.6291 -0.4992 -0.1664 0.6379 0.7577
3.2 -0.3306 -0.7023 -0.5736 -0.2962 0.5969 0.7400
3.4 -0.3628 -0.7766 -0.6468 -0.4249 0.4626 0.7211
3.6 -0.3939 -0.8509 -0.7211 -0.5547 0.3251 0.7023
</tableData>
</table>
</propeller>