- Oct 18, 2003
- Saline Michigan
It does look like a place where it will see errors based upon g loading and angle of attack.So here's question: After watching the latest video with the duct taped dam in front of the static port on the bottom of the fuselage.
Is it possible to put a static port on the bottom of the fuselage (or wing)? I always assumed that on the bottom of the wing would be subject to high pressure and the same (to a point) for the bottom of the fuselage. Also would be subject to variations in pressure due to changes in AOA.
In all the static ports I've looked at, I've never seen one on the bottom of the plane. Always on the side of the fuselage (or on a pitot tube mast).