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fgdata/Aircraft/c172p/Engines/prop_76in2f_NACA_15-25deg.xml
Stuart Buchanan 1ab65221b1 Final V3.6.0 version of c172p-detailed.
https://github.com/Juanvvc/c172p-detailed
commit 874b89fedff35dfe1967e09365d3cb0d5b11522c
2015-07-24 18:37:16 +01:00

62 lines
2.3 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>