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Flap drag fixes. The meaning of the drag number has changed, so the

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values must too.
This commit is contained in:
aross 2002-06-15 03:40:46 +00:00
parent 53809e0937
commit 6fd1e02f65
6 changed files with 37 additions and 36 deletions
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6
Aircraft-yasim/747.xml
View file

@ -25,8 +25,8 @@
<wing x="-26.50" y="3.01" z="-1.45" length="33.72" chord="13.25" sweep="33"
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"/>
<flap0 start="0" end=".56" lift="1.8" drag="1.2"/>
<flap1 start=".64" end=".88" lift="1.3" drag="1.2"/>
<slat start="0" end="1" aoa="2" drag="1.1"/>
<spoiler start="0.2" end="0.6" lift="0.3" drag="2.0"/>
<control-input axis="/controls/flaps" control="FLAP0"/>
@ -45,7 +45,7 @@
<hstab x="-62.63" y="1.81" z="1.81" chord="8.43" length="10.84" taper=".29"
sweep="28" dihedral="7" camber="-0.1" effectiveness="1.5">
<stall aoa="15" width="2" peak="1.5"/>
<flap0 start="0" end="1" lift="1.6" drag="1.8"/>
<flap0 start="0" end="1" lift="1.6" drag="1.2"/>
<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"/>

35
Aircraft-yasim/a4.xml
View file

@ -1,4 +1,4 @@
<airplane mass="10250">
<airplane mass="9853">
<!-- Approach configuration -->
<approach speed="130" aoa="13.5">
@ -7,9 +7,9 @@
<control-setting axis="/controls/gear-down" value="1"/>
</approach>
<!-- Cruise configuration -->
<cruise speed="517" alt="34000">
<control-setting axis="/controls/throttle[0]" value="1.0"/>
<!-- Cruise configuration. This number is for an A-4F (595mph/FL340) -->
<cruise speed="585" alt="34000">
<control-setting axis="/controls/throttle[0]" value="0.8"/>
<control-setting axis="/controls/flaps" value="0.0"/>
<control-setting axis="/controls/gear-down" value="0"/>
</cruise>
@ -20,9 +20,9 @@
width="2.0" taper="0.5" midpoint="0.3"/>
<wing x="-6.4" y=".55" z="0" taper=".186"
length="4.04" chord="3.95" sweep="28" dihedral="0" camber="0.1">
length="4.04" chord="3.95" sweep="28" dihedral="0" camber="0.02">
<stall aoa="27" width="10" peak="1.3"/>
<flap0 start="0.0" end="0.5" lift="1.5" drag="2.0"/>
<flap0 start="0.0" end="0.5" lift="1.4" drag="1.2"/>
<flap1 start="0.5" end="1.0" lift="1.25" drag="1.3"/>
<control-input axis="/controls/flaps" control="FLAP0"/>
<control-input axis="/controls/aileron" control="FLAP1" split="true"/>
@ -37,7 +37,7 @@
<hstab x="-11.01" y="0" z="1.38" taper=".3" effectiveness="1.99"
length="2.02" chord="2.02" sweep="26">
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0" end="1" lift="1.7" drag="2.0"/>
<flap0 start="0" end="1" lift="1.7" drag="1.2"/>
<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"/>
@ -46,22 +46,21 @@
<vstab x="-11.01" y="0" z="1.38" taper=".176"
length="2.57" chord="3.11" sweep="28" effectiveness="1.5">
<stall aoa="27" width="10" peak="1.5"/>
<flap0 start="0" end="1" lift="1.15" drag="1.3"/>
<flap0 start="0" end="1" lift="1.15" drag="1.2"/>
<control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"
min="1" max="-1"/>
</vstab>
<!-- NOTE: Skyhawks do NOT have afterburners. This one does for
testing purposes only -->
<jet x="-5.0" y="0" z=".44" mass="2050" thrust="10250" afterburner="16500">
<!-- P&W J52-P-6A turbojet, 8500 lbs sea level thrust -->
<jet x="-5.0" y="0" z=".44" mass="1800" thrust="8500">
<control-input axis="/controls/throttle[0]" control="THROTTLE"/>
<control-input axis="/controls/afterburner[0]" control="REHEAT"/>
</jet>
<!-- nose -->
<gear x="-2.29" y="0" z="-1.93" retract-time="7" compression=".96">
<control-input axis="/controls/rudder" control="STEER" square="true"/>
<control-input axis="/controls/rudder" control="STEER" square="true"
src0="-1" src1="1" dst0="-0.9" dst1="0.9"/>
<control-input axis="/controls/gear-down" control="EXTEND"/>
<control-output control="EXTEND" prop="/gear/gear[0]/position-norm"/>
<control-speed control="EXTEND" transition-time="7"/>
@ -87,12 +86,14 @@
one in each wing and one behind the cockpit. TA-4F had "only" 100
gallons in the fuselage due to the second seat, so the wings must
have 0-350 gallons each. Call the tanks 260/280/260 gallons, and
use 6.72 lbs/gal for Jet-A fuel. -->
<tank x="-5.50" y="0" z="0.5" jet="true" capacity="1880"/>
use 6.72 lbs/gal for Jet-A fuel. BUT: this is an A-4E, which had
770 gallons. Figure that the extra 30 all went into the expanded
center tank. -->
<tank x="-5.50" y="0" z="0.5" jet="true" capacity="1678"/>
<tank x="-6.0" y="1" z="0" jet="true" capacity="1750"/>
<tank x="-6.0" y="-1" z="0" jet="true" capacity="1750"/>
<ballast x="-1.5" y="0" z="1" mass="650"/> <!-- cockpit -->
<ballast x="-3.0" y="0" z="1" mass="650"/> <!-- cockpit -->
<ballast x="-1.5" y="0" z="1" mass="450"/> <!-- cockpit -->
<ballast x="-3.0" y="0" z="1" mass="450"/> <!-- cockpit -->
</airplane>

8
Aircraft-yasim/c172.xml
View file

@ -22,8 +22,8 @@
<wing x="-2.47" y=".51" z=".68" taper=".78"
length="5.37" chord="1.54" sweep="0" dihedral="1" camber="0.1">
<stall aoa="16" width="6" peak="1.5"/>
<flap0 start="0" end=".38" lift="1.6" drag="2.0"/>
<flap1 start=".78" end="1" lift="1.5" drag="1.6"/>
<flap0 start="0" end=".38" lift="1.5" drag="1.2"/>
<flap1 start=".78" end="1" lift="1.5" drag="1.2"/>
<control-input axis="/controls/flaps" control="FLAP0"/>
<control-input axis="/controls/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/>
@ -38,7 +38,7 @@
<hstab x="-7.16" y="0.08" z=".17" taper=".63"
length="1.71" chord="1.36" sweep="0">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.7" drag="2.0"/>
<flap0 start="0" end="1" lift="1.7" drag="1.2"/>
<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"/>
@ -47,7 +47,7 @@
<vstab x="-7.16" y="0" z=".17" taper=".5"
length="1.71" chord="1.54" sweep="20">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.3" drag="1.5"/>
<flap0 start="0" end="1" lift="1.3" drag="1.2"/>
<control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"

8
Aircraft-yasim/c310.xml
View file

@ -29,8 +29,8 @@
<wing x="-3.65" y="0.62" z="-0.18" length ="4.68" chord ="1.68"
sweep="0" dihedral="5" taper="0.8" camber="0.1">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end=".5" lift="1.5" drag="2.0"/>
<flap1 start=".55" end=".94" lift="1.3" drag="1.5"/>
<flap0 start="0" end=".5" lift="1.5" drag="1.2"/>
<flap1 start=".55" end=".94" lift="1.3" drag="1.2"/>
<control-input axis="/controls/flaps" control="FLAP0"/>
<control-speed control="FLAP0" transition-time="5"/>
<control-output control="FLAP0" prop="/surface-positions/flap-pos-norm"/>
@ -45,7 +45,7 @@
<hstab x="-8.33" y="0.22" z="0.07" length ="2.34" chord ="1.24"
sweep="0" dihedral="0" taper="0.6">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.68" drag="1.8"/>
<flap0 start="0" end="1" lift="1.68" drag="1.2"/>
<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"/>
@ -54,7 +54,7 @@
<vstab x="-8.26" y="0.00" z="0.26" length ="2.16" chord ="1.61"
sweep="36" taper="0.5">
<stall aoa="16" width="4" peak="1.5"/>
<flap0 start="0" end="1" lift="1.3" drag="1.5"/>
<flap0 start="0" end="1" lift="1.3" drag="1.2"/>
<control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>

8
Aircraft-yasim/dc3.xml
View file

@ -31,8 +31,8 @@
<wing x="-7.02" y="1.09" z="0.95" length="11.58" camber="0.1"
chord="4.77" taper=".286" sweep="19" dihedral="4">
<stall aoa="14" width="3" peak="1.5"/>
<flap0 start="0.04" end="0.38" lift="1.5" drag="2.0"/>
<flap1 start="0.38" end="0.97" lift="1.2" drag="1.5"/>
<flap0 start="0.04" end="0.38" lift="1.5" drag="1.2"/>
<flap1 start="0.38" end="0.97" lift="1.2" drag="1.2"/>
<control-input axis="/controls/flaps" control="FLAP0"/>
<control-input axis="/controls/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/>
@ -47,7 +47,7 @@
<hstab x="-18.12" y="0.41" z="0.27" length="3"
chord="3" taper=".545" sweep="15">
<stall aoa="14" width="3" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
<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"/>
@ -56,7 +56,7 @@
<vstab x="-18.12" y="0" z="0.95" length="2.72"
chord="3.95" taper=".462" sweep="2">
<stall aoa="14" width="3" peak="1.5"/>
<flap0 start="0" end="1" lift="1.5" drag="2.0"/>
<flap0 start="0" end="1" lift="1.5" drag="1.2"/>
<control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"/>

8
Aircraft-yasim/harrier.xml
View file

@ -27,8 +27,8 @@
<wing x="-7.32" y="0.46" z="0.93" length="3.71" chord="3.15"
taper=".294" sweep="28" dihedral="-11" camber="0.05">
<stall aoa="21" width="8" peak="1.3"/>
<flap0 start="0.11" end="0.56" lift="1.5" drag="2.0"/>
<flap1 start="0.56" end="0.91" lift="1.2" drag="1.5"/>
<flap0 start="0.11" end="0.56" lift="1.5" drag="1.2"/>
<flap1 start="0.56" end="0.91" lift="1.2" drag="1.2"/>
<control-input axis="/controls/flaps" control="FLAP0"/>
<control-input axis="/controls/aileron" control="FLAP1" split="true"/>
<control-input axis="/controls/aileron-trim" control="FLAP1" split="true"/>
@ -42,7 +42,7 @@
<hstab x="-12.23" y="0.00" z="0.93" length="2.04" chord="1.48"
taper=".313" sweep="24.5" dihedral="-12">
<stall aoa="20" width="7" peak="1.5"/>
<flap0 start="0" end="1" lift="1.7" drag="2.0"/>
<flap0 start="0" end="1" lift="1.7" drag="1.2"/>
<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"/>
@ -51,7 +51,7 @@
<vstab x="-12.51" y="0.00" z="1.20" length="2.78" chord="2.41"
taper=".308" sweep="23.5">
<stall aoa="20" width="7" peak="1.5"/>
<flap0 start="0.12" end="0.88" lift="1.2" drag="1.5"/>
<flap0 start="0.12" end="0.88" lift="1.2" drag="1.2"/>
<control-input axis="/controls/rudder" control="FLAP0" invert="true"/>
<control-input axis="/controls/rudder-trim" control="FLAP0" invert="true"/>
<control-output control="FLAP0" prop="/surface-positions/rudder-pos-norm"