Keith103June 18, 2018, 5:25pm
My whole project is geared for operating the airplane out of an enclosed trailer.
I was looking for a location for the pitot head which will cause least damage to the pitot tube. Is the following placement at wing tip an acceptable way to go? if the tube sticks out any longer, the storage area in the trailer for the wings has to be wider just for this small tube which is sticking out.
The actual pitot opening is likely to be about 2 to 3 inches away from the closest surface of wing.
I am assuming that the airflow is disturbed the most at the first few inches closest to the wing surface.
This makes the flexible tubing connection to the ASI about 14 feet long.
Is this too long a tube, meaning will the dynamic pressure decay over such a long tube leading to reduced read out ?
Thanks for any suggestions / comments.

I was looking for a location for the pitot head which will cause least damage to the pitot tube. Is the following placement at wing tip an acceptable way to go? if the tube sticks out any longer, the storage area in the trailer for the wings has to be wider just for this small tube which is sticking out.
The actual pitot opening is likely to be about 2 to 3 inches away from the closest surface of wing.
I am assuming that the airflow is disturbed the most at the first few inches closest to the wing surface.
This makes the flexible tubing connection to the ASI about 14 feet long.
Is this too long a tube, meaning will the dynamic pressure decay over such a long tube leading to reduced read out ?
Thanks for any suggestions / comments.




