2016-11-04 22:13:12 +00:00
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<?xml version="1.0"?>
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<!--
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File: V2522_A5.xml
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Author: Aero-Matic v 0.81
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Inputs:
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name: V2522_A5
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type: turbine
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thrust: 21998.928 lb
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augmented? no
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injected? no
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-->
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2016-11-05 03:39:28 +00:00
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<turbine_engine name="V2527_A5">
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2016-11-06 16:03:42 +00:00
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<milthrust> 26600 </milthrust>
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2016-11-07 15:39:53 +00:00
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<bypassratio> 2.0 </bypassratio>
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2016-11-04 22:13:12 +00:00
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<tsfc> 0.8 </tsfc>
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<bleed> 0.03</bleed>
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2016-11-05 03:39:28 +00:00
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<idlen1> 23.4 </idlen1>
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<idlen2> 63.7 </idlen2>
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<maxn1> 105.8 </maxn1>
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<maxn2> 112.5 </maxn2>
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2016-11-04 22:13:12 +00:00
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<augmented> 0 </augmented>
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<injected> 0 </injected>
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<function name="IdleThrust">
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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-10000 0 10000 20000 30000 40000 50000
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0.0 0.0430 0.0488 0.0528 0.0694 0.0899 0.1183 0.1467
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0.2 0.0500 0.0501 0.0335 0.0544 0.0797 0.1049 0.1342
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0.4 0.0040 0.0047 0.0020 0.0272 0.0595 0.0891 0.1203
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0.6 0.0 0.0 0.0 0.0 0.0276 0.0718 0.1073
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0.8 0.0 0.0 0.0 0.0 0.0474 0.0868 0.0900
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1.0 0.0 0.0 0.0 0.0 0.0 0.0552 0.0800
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</tableData>
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</table>
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</function>
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<function name="MilThrust">
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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-10000 0 10000 20000 30000 40000 50000
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0.0 1.2600 1.0000 0.7400 0.5340 0.3720 0.2410 0.1490
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0.2 1.1710 0.9340 0.6970 0.5060 0.3550 0.2310 0.1430
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0.4 1.1500 0.9210 0.6920 0.5060 0.3570 0.2330 0.1450
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0.6 1.1810 0.9510 0.7210 0.5320 0.3780 0.2480 0.1540
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0.8 1.2580 1.0200 0.7820 0.5820 0.4170 0.2750 0.1700
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1.0 1.3690 1.1200 0.8710 0.6510 0.4750 0.3150 0.1950
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1.2 1.4850 1.2300 0.9750 0.7440 0.5450 0.3640 0.2250
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1.4 1.5941 1.3400 1.0860 0.8450 0.6280 0.4240 0.2630
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</tableData>
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</table>
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</function>
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</turbine_engine>
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