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fgdata/Aircraft/c172p/Engines/prop_75in_2f_NACA_15-30deg.xml

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<?xml version="1.0"?>
<!--
Diameter: 75 in (1.91 m)
Calculated blade angle: at 75% of the radius
Data from NACA Report 640 : http://naca.central.cranfield.ac.uk/reports/1938/naca-report-640.pdf
-->
<propeller name="variable-Pitch 75-inch Two-Blade Propeller" version="1.1">
<ixx> 1.67 </ixx>
<diameter unit="IN"> 75.0 </diameter>
<numblades> 2 </numblades>
<minpitch> 15 </minpitch>
<maxpitch> 30 </maxpitch>
<table name="C_THRUST" type="internal">
<tableData>
15 20 25 30
0 0.0990 0.1040 0.1125 0.1175
0.1 0.0950 0.1040 0.1100 0.1170
0.2 0.0880 0.1030 0.1075 0.1150
0.3 0.0780 0.1010 0.1060 0.1125
0.4 0.0645 0.0930 0.1055 0.1100
0.5 0.0495 0.0820 0.1045 0.1080
0.6 0.0340 0.0700 0.0970 0.1075
0.7 0.0185 0.0550 0.0870 0.1075
0.8 0.0040 0.0390 0.0750 0.1040
0.9 -0.0160 0.0240 0.0600 0.0950
1 -0.0300 0.0060 0.0450 0.0825
1.1 -0.0400 -0.0140 0.0300 0.0695
1.2 -0.0500 -0.0330 0.0150 0.0540
1.3 -0.0550 -0.0450 -0.0010 0.0380
1.4 -0.06 -0.0550 -0.0130 0.0225
1.5 -0.0650 -0.0600 -0.0250 0.0075
1.6 -0.0700 -0.0650 -0.0380 -0.0090
2 -0.0750 -0.0720 -0.0700 -0.0550
3 -0.0800 -0.0800 -0.0900 -0.1000
</tableData>
</table>
<table name="C_POWER" type="internal">
<tableData>
15 20 25 30
0 0.0400 0.0660 0.1080 0.1420
0.1 0.0406 0.0650 0.1060 0.1405
0.2 0.0406 0.0640 0.1020 0.1380
0.3 0.0400 0.0625 0.0975 0.1360
0.4 0.0366 0.0600 0.0910 0.1330
0.5 0.0318 0.0580 0.0860 0.1280
0.6 0.0250 0.0540 0.0825 0.1230
0.7 0.0160 0.0475 0.0790 0.1180
0.8 0.0050 0.0370 0.0730 0.1140
0.9 -0.0067 0.0260 0.0640 0.1080
1 -0.0150 0.0100 0.0520 0.1000
1.1 -0.0200 0.0000 0.0375 0.0895
1.2 -0.0250 -0.0100 0.0220 0.0750
1.3 -0.0270 -0.0200 0.0040 0.0580
1.4 -0.0285 -0.0278 -0.02 0.0380
1.5 -0.0300 -0.0350 -0.0400 0.0180
1.6 -0.0315 -0.0390 -0.0530 -0.0070
2 -0.0330 -0.0500 -0.0750 -0.0750
3 -0.0350 -0.0550 -0.1000 -0.1200
</tableData>
</table>
</propeller>