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Updated with Andy's latest fix for 747.

This commit is contained in:
jimw 2002-06-03 19:52:51 +00:00
parent 901e2a9212
commit 36f9127650

View file

@ -10,9 +10,9 @@
</approach>
<!-- Cruise configuration -->
<cruise speed="530" alt="41000">
<control-setting axis="/controls/throttle[0]" value="1.0"/>
<control-setting axis="/controls/throttle[1]" value="1.0"/>
<cruise speed="490" alt="36000">
<control-setting axis="/controls/throttle[0]" value="0.75"/>
<control-setting axis="/controls/throttle[1]" value="0.75"/>
<control-setting axis="/controls/flaps" value="0.0"/>
<control-setting axis="/controls/gear-down" value="0"/>
</cruise>
@ -23,7 +23,7 @@
width="6" taper="0.3" midpoint="0.2"/>
<wing x="-26.50" y="3.01" z="-1.45" length="33.72" chord="13.25" sweep="33"
taper=".27" dihedral="7" camber="0.1">
taper=".27" dihedral="7" camber="0.15" incidence="-0.7">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end=".56" lift="1.8" drag="3"/>
<flap1 start=".64" end=".88" lift="1.3" drag="1.5"/>
@ -43,9 +43,9 @@
</wing>
<hstab x="-62.63" y="1.81" z="1.81" chord="8.43" length="10.84" taper=".29"
sweep="28" dihedral="7" effectiveness="1.9">
sweep="28" dihedral="7" camber="-0.1" effectiveness="1.5">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" lift="1.4" drag="1.8"/>
<flap0 start="0" end="1" lift="1.6" drag="1.8"/>
<control-input axis="/controls/elevator" control="FLAP0"/>
<control-input axis="/controls/elevator-trim" control="FLAP0"/>
<control-output control="FLAP0" prop="/surface-positions/elevator-pos-norm"/>
@ -61,19 +61,22 @@
min="1" max="-1"/>
</vstab>
<jet x="-34.93" y="16.26" z="-1.20" mass="8000" thrust="60000">
<!-- The CF6 engines are rated at 60000 lbs thrust, flat rated to 33 -->
<!-- degrees C. Corrected to YASim's standard atmosphere temperature -->
<!-- of 288.2 kelvins, that gives 63737 lbs of nominal thrust. -->
<jet x="-34.93" y="16.26" z="-1.20" mass="8000" thrust="63737">
<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
</jet>
<jet x="-26.50" y="12.65" z="-2.41" mass="8000" thrust="60000">
<jet x="-26.50" y="12.65" z="-2.41" mass="8000" thrust="63737">
<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
</jet>
<jet x="-26.50" y="-12.65" z="-2.41" mass="8000" thrust="60000">
<jet x="-26.50" y="-12.65" z="-2.41" mass="8000" thrust="63737">
<control-input axis="/controls/throttle[1]" control="THROTTLE"/>
</jet>
<jet x="-34.93" y="-16.26" z="-1.20" mass="8000" thrust="60000">
<jet x="-34.93" y="-16.26" z="-1.20" mass="8000" thrust="63737">
<control-input axis="/controls/throttle[1]" control="THROTTLE"/>
</jet>