andrewarles
08-21-2014, 06:58 AM
Hi,
I've been looking at the excellent home cockpit web site at http://www.flaps2approach.com
It says that the pitch pressure on a B737 is designed to be 37 pounds +-4.
Am I correct in assuming that it's a constant/linear pressure through the full movement when there is no airflow over the wings and, that when the aircraft is flying the pressure increases with the pitch angle?
Thanks
Andrew
I've been looking at the excellent home cockpit web site at http://www.flaps2approach.com
It says that the pitch pressure on a B737 is designed to be 37 pounds +-4.
Am I correct in assuming that it's a constant/linear pressure through the full movement when there is no airflow over the wings and, that when the aircraft is flying the pressure increases with the pitch angle?
Thanks
Andrew