diff --git a/Aircraft-yasim/j3cub.xml b/Aircraft-yasim/j3cub.xml index b96d28624..1fcc362ad 100644 --- a/Aircraft-yasim/j3cub.xml +++ b/Aircraft-yasim/j3cub.xml @@ -41,7 +41,7 @@ since it is what the weight-and-balance site above uses. <cruise speed="64" alt="0"> <control-setting axis="/controls/throttle[0]" value="0.75"/> <control-setting axis="/controls/mixture[0]" value="0.75"/> - <control-setting axis="/controls/elevator" value="0.1"/> + <control-setting axis="/controls/elevator-trim" value="0.1"/> </cruise> <!-- pilot's eyepoint --> @@ -59,9 +59,9 @@ since it is what the weight-and-balance site above uses. Note that the J3 Cub has no flaps. With a stall speed of 25kt, who needs them? From what I've read, the ailerons add lots of drag. --> -<wing x="-0.80" y="0.42" z="0.0" taper="1.0" incidence="2" twist="-2" +<wing x="-0.80" y="0.42" z="0.0" taper="1.0" incidence="2" twist="-3" length="4.87" chord="1.60" sweep="0" dihedral="5" camber="0.1"> - <stall aoa="17" width="2" peak="1.5"/> + <stall aoa="18" width="4" peak="1.5"/> <flap0 start=".31" end="0.85" lift="1.5" drag="1.4"/> <control-input axis="/controls/aileron" control="FLAP0" split="true"/> <control-input axis="/controls/aileron-trim" control="FLAP0" split="true"/> @@ -74,7 +74,7 @@ since it is what the weight-and-balance site above uses. <hstab x="-4.87" y="0.05" z="-0.42" taper="0.8" effectiveness="1.24" length="1.49" chord="1.13" sweep="0"> <stall aoa="16" width="4" peak="1.5"/> - <flap0 start="0" end="1" lift="1.5" drag="1.2"/> + <flap0 start="0" end="1" lift="1.4" 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"/> @@ -130,6 +130,8 @@ since it is what the weight-and-balance site above uses. weight-and-balance page cited at the start. --> +<ballast x="-4.0" y="0" z="-0.70" mass="-75"/> + <!-- pilot --> <weight x="-0.91" y="0" z="-0.70" mass-prop="/yasim/j3cub/pilot-lb"/>