62 lines
1.3 KiB
XML
62 lines
1.3 KiB
XML
|
<?xml version="1.0"?>
|
||
|
|
||
|
<!--
|
||
|
Diameter: 76 in (1.93 m)
|
||
|
Pitch: 62.5 in
|
||
|
Calculated blade angle: 20° at 75% of the radius
|
||
|
Data from NACA Report 640 : http://naca.central.cranfield.ac.uk/reports/1938/naca-report-640.pdf
|
||
|
-->
|
||
|
|
||
|
<propeller name="NACA 640 (5868-9) 76-inch 20deg Two-Blade Propeller">
|
||
|
<ixx> 1.67 </ixx>
|
||
|
<diameter unit="IN"> 76.0 </diameter>
|
||
|
<numblades> 2 </numblades>
|
||
|
<minpitch> 20 </minpitch>
|
||
|
<maxpitch> 20 </maxpitch>
|
||
|
|
||
|
<table name="C_THRUST" type="internal">
|
||
|
<tableData>
|
||
|
0 0.1040
|
||
|
0.1 0.1040
|
||
|
0.2 0.1030
|
||
|
0.3 0.1010
|
||
|
0.4 0.0930
|
||
|
0.5 0.0820
|
||
|
0.6 0.0700
|
||
|
0.7 0.0550
|
||
|
0.8 0.0390
|
||
|
0.9 0.0240
|
||
|
1 0.0060
|
||
|
1.1 -0.0140
|
||
|
1.2 -0.0330
|
||
|
1.3 -0.0450
|
||
|
1.5 -0.0600
|
||
|
2 -0.0720
|
||
|
3 -0.0800
|
||
|
</tableData>
|
||
|
</table>
|
||
|
|
||
|
<table name="C_POWER" type = "internal">
|
||
|
<tableData>
|
||
|
0 0.0660
|
||
|
0.1 0.0650
|
||
|
0.2 0.0640
|
||
|
0.3 0.0625
|
||
|
0.4 0.0600
|
||
|
0.5 0.0580
|
||
|
0.6 0.0540
|
||
|
0.7 0.0475
|
||
|
0.8 0.0370
|
||
|
0.9 0.0260
|
||
|
1 0.0100
|
||
|
1.1 0.0000
|
||
|
1.2 -0.0100
|
||
|
1.3 -0.0200
|
||
|
1.5 -0.0350
|
||
|
2 -0.0500
|
||
|
3 -0.0550
|
||
|
</tableData>
|
||
|
</table>
|
||
|
|
||
|
</propeller>
|