so, i was wondering, how does one determine
the forward/aft center of gravity
for a multi-engine aircraft model?
for the sake of argument, let's just say
that specifications are next to nil,
except that, there are decent 3 view drawings
with height, length and wing span dimensions.
the forward/aft center of gravity
for a multi-engine aircraft model?
for the sake of argument, let's just say
that specifications are next to nil,
except that, there are decent 3 view drawings
with height, length and wing span dimensions.