Hi Netters.
It was my impression that the static port location should be at the widest
part of the fuselage.The must be one on each side and they are
interconnected. This is done because if yopu apply a bit of rudder and yaw
the plane , the port on one side moves into the slipstream and raises the
pressure while the port on the other side of the fuselage moves back out of
the slipstream thus reducing the pressure. By interconnecting these two an
average pressure is maintained.
If you use only inside cabin pressure the difference between inside and
outside can be variable because if you open a hot or cold air vent you
change the pressure. An increase in speed may change the interior pressure
of the cabin. These changes will make the differential pressure between the
ram air and the average pressures inaccurate and variable.
Any suggestions?
Regards'
Harold Woods
Orillia,ON,Can.
haroldwo...@rogers.com
