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fgdata/Aircraft/c172p/Engines/prop_76in2f_NACA_15-25deg.xml
Stuart Buchanan 88b49b4259 Sync c172p with c172p-detailed master branch.
Sync with commit cab40a0af989bf08302836f98e91672920369fa3
2015-07-05 19:32:41 +01:00

61 lines
2 KiB
XML

<?xml version="1.0"?>
<!--
Diameter: 76 in (1.93 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="15 -25 deg NACA 640 (5868-9) 76-inch Two-Blade Propeller">
<ixx> 1.67 </ixx>
<diameter unit="IN"> 76.0 </diameter>
<numblades> 2 </numblades>
<minpitch> 15 </minpitch>
<maxpitch> 25 </maxpitch>
<table name="C_THRUST" type="internal">
<tableData>
15 20 25
0 0.0990 0.1040 0.1125
0.1 0.0950 0.1040 0.1100
0.2 0.0880 0.1030 0.1075
0.3 0.0780 0.1010 0.1060
0.4 0.0645 0.0930 0.1055
0.5 0.0495 0.0820 0.1045
0.6 0.0340 0.0700 0.0970
0.7 0.0185 0.0550 0.0870
0.8 0.0040 0.0390 0.0750
0.9 -0.0160 0.0240 0.0600
1 -0.0300 0.0060 0.0450
1.1 -0.0400 -0.0140 0.0300
1.2 -0.0500 -0.0330 0.0150
1.3 -0.0550 -0.0450 -0.0010
1.5 -0.0650 -0.0600 -0.0250
2 -0.0750 -0.0720 -0.0750
3 -0.0800 -0.0800 -0.0900
</tableData>
</table>
<table name="C_POWER" type = "internal">
<tableData>
15 20 25
0 0.0400 0.0660 0.1080
0.1 0.0406 0.0650 0.1060
0.2 0.0406 0.0640 0.1020
0.3 0.0400 0.0625 0.0975
0.4 0.0366 0.0600 0.0910
0.5 0.0318 0.0580 0.0860
0.6 0.0250 0.0540 0.0825
0.7 0.0160 0.0475 0.0790
0.8 0.0050 0.0370 0.0730
0.9 -0.0067 0.0260 0.0640
1 -0.0150 0.0100 0.0520
1.1 -0.0200 0.0000 0.0375
1.2 -0.0250 -0.0100 0.0220
1.3 -0.0270 -0.0200 0.0040
1.5 -0.0300 -0.0350 -0.0450
2 -0.0330 -0.0500 -0.0750
</tableData>
</table>
</propeller>