Tue Feb 05, 2019 2:59 pm #1671996
Altimeter accuracy depends on static port position
Air flow parallel to static port.
Wrong static port position will cause altimeter shows change in altitude when aircraft speed("airspeed") increase although the plane is flying at the same height.(because of bernoulli effect)
How find neutral static port position on fuselage where airflow will not disturb altimeter accuracy, (like do in my video)?
And how desing static port holes to avoid this problem?