Small JSBSim cleanup.

parent e40393f2
<?xml version="1.0" encoding="UTF-8"?>
<aerodynamics file="aero.xml">
<aero_ref_pt_shift_x>
<function name="aero/coefficient/kC0"><description>Focus shift due to Mach [MAC]</description>
<table><!-- [Bliznyuk p. 51, upper plot]-->
<independentVar>velocities/mach</independentVar>
<tableData>
0.18 0.457
0.66 0.464
0.72 0.466
0.77 0.471
0.81 0.476
0.88 0.492
0.93 0.506
1.04 0.561
1.07 0.569
1.10 0.574
1.17 0.577
1.24 0.577
1.39 0.570
3.0 0.493
</tableData>
</table>
</function>
</aero_ref_pt_shift_x>
<function name="aero/coefficient/Kmax">
<description>Maximum lift to drag ratio</description>
<product>
<value>6.99</value><!-- = 8.0/1.145 --><!-- M = 2.2 K = 8.0 [Bliznyuk p.67]-->
<table><!-- Normalised Kmax [Bliznyuk p.49]-->
<independentVar>velocities/mach</independentVar>
<tableData>
0.60 1.865
0.80 1.830
0.85 1.810
0.90 1.770
1.00 1.600
1.20 1.320
1.40 1.175
1.60 1.100
1.80 1.060
2.00 1.050
2.40 1.040
</tableData>
</table>
</product>
</function>
</aerodynamics>
......@@ -166,21 +166,6 @@
</product>
</function>
<function name="aero/inlet-pressure-recovery">
<table><!-- [Bliznyuk p. 112] In TsAGI definition (\sigma_{st}) -->
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 0.9
0.7 0.97
0.85 0.97
1.2 0.97
1.8 0.94
2.0 0.92
2.2 0.9
</tableData>
</table>
</function>
<!-- LIFT -->
......
......@@ -38,7 +38,6 @@
<property>atmosphere/T-degC</property>
<property>atmosphere/T-stag-diff-K</property>
<property>aero/qimpact-atm</property>
<property>aero/inlet-pressure-recovery</property>
<property>fcs/surfaces/gravity-z-norm</property>
......@@ -330,9 +329,21 @@
<product>
<p>&U;/efficiency-norm</p>
<p>aero/qimpact-atm</p>
<p>aero/inlet-pressure-recovery</p>
<table>
<!-- [Bliznyuk p. 112] Pressure recovery In TsAGI definition (\sigma_{st}) -->
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 0.9
0.7 0.97
0.85 0.97
1.2 0.97
1.8 0.94
2.0 0.92
2.2 0.9
</tableData>
</table>
</product>
</sum>
</sum>
</function>
</fcs_function>
......
......@@ -38,7 +38,6 @@
<property>atmosphere/T-degC</property>
<property>atmosphere/T-stag-diff-K</property>
<property>aero/qimpact-atm</property>
<property>aero/inlet-pressure-recovery</property>
<property>fcs/surfaces/gravity-z-norm</property>
......@@ -330,9 +329,21 @@
<product>
<p>&U;/efficiency-norm</p>
<p>aero/qimpact-atm</p>
<p>aero/inlet-pressure-recovery</p>
<table>
<!-- [Bliznyuk p. 112] Pressure recovery In TsAGI definition (\sigma_{st}) -->
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 0.9
0.7 0.97
0.85 0.97
1.2 0.97
1.8 0.94
2.0 0.92
2.2 0.9
</tableData>
</table>
</product>
</sum>
</sum>
</function>
</fcs_function>
......
......@@ -38,7 +38,6 @@
<property>atmosphere/T-degC</property>
<property>atmosphere/T-stag-diff-K</property>
<property>aero/qimpact-atm</property>
<property>aero/inlet-pressure-recovery</property>
<property>fcs/surfaces/gravity-z-norm</property>
......@@ -330,9 +329,21 @@
<product>
<p>&U;/efficiency-norm</p>
<p>aero/qimpact-atm</p>
<p>aero/inlet-pressure-recovery</p>
<table>
<!-- [Bliznyuk p. 112] Pressure recovery In TsAGI definition (\sigma_{st}) -->
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 0.9
0.7 0.97
0.85 0.97
1.2 0.97
1.8 0.94
2.0 0.92
2.2 0.9
</tableData>
</table>
</product>
</sum>
</sum>
</function>
</fcs_function>
......
......@@ -38,7 +38,6 @@
<property>atmosphere/T-degC</property>
<property>atmosphere/T-stag-diff-K</property>
<property>aero/qimpact-atm</property>
<property>aero/inlet-pressure-recovery</property>
<property>fcs/surfaces/gravity-z-norm</property>
......@@ -330,9 +329,21 @@
<product>
<p>&U;/efficiency-norm</p>
<p>aero/qimpact-atm</p>
<p>aero/inlet-pressure-recovery</p>
<table>
<!-- [Bliznyuk p. 112] Pressure recovery In TsAGI definition (\sigma_{st}) -->
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.0 0.9
0.7 0.97
0.85 0.97
1.2 0.97
1.8 0.94
2.0 0.92
2.2 0.9
</tableData>
</table>
</product>
</sum>
</sum>
</function>
</fcs_function>
......
<?xml version="1.0" encoding="UTF-8"?>
<system name="Tu-144 Fuel system" file="fuel.xml">
<channel name="Trim"><!-- [Bliznyuk p. 51, upper plot] -->
<fcs_function name="systems/fuel/cg-min">
<description>Minimal CG for fuel pumping</description>
<function>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.938 0.398
1.030 0.446
</tableData>
</table>
</function>
</fcs_function>
<fcs_function name="systems/fuel/cg-max">
<description>Maximal CG for fuel pumping</description>
<function>
<table>
<independentVar lookup="row">velocities/mach</independentVar>
<tableData>
0.932 0.418
1.034 0.470
</tableData>
</table>
</function>
</fcs_function>
</channel>
</system>
......@@ -61,7 +61,7 @@
</test>
</switch>
-->
</channel>
......
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