An aeroplane of m × 104kg mass is designed with the line of thrust n × 10-1m above the line of drag. In routine flight t
Posted: Wed May 18, 2022 6:23 am
An aeroplane of m × 104kg
mass is designed with the line of thrust n
× 10-1m above the line of drag. In
routine flight the drag is 15.2 kN, and the centre of pressure
on the main plane is 200 mm behind the centre of mass. If the
centre of pressure on the tailplane is 12 m behind the centre
of mass, what is the lift from the tailplane
(FTPTP)?
mass is designed with the line of thrust n
× 10-1m above the line of drag. In
routine flight the drag is 15.2 kN, and the centre of pressure
on the main plane is 200 mm behind the centre of mass. If the
centre of pressure on the tailplane is 12 m behind the centre
of mass, what is the lift from the tailplane
(FTPTP)?