A fixed-wing aircraft has a mass of 2000 kg, center of lift and center of gravity are in the same vertical straight line
Posted: Tue Jun 07, 2022 5:56 pm
A fixed-wing aircraft has a mass of 2000 kg, center of lift and
center of gravity are in the same vertical straight line when in
normal cruising flight. If the thrust is 4.5 kN, and is 180 mm
below the center of drag, what force (in N) must there be on the
tail plane which is 6 m behind the center of gravity? Indicate only
the numeric value of your response.
center of gravity are in the same vertical straight line when in
normal cruising flight. If the thrust is 4.5 kN, and is 180 mm
below the center of drag, what force (in N) must there be on the
tail plane which is 6 m behind the center of gravity? Indicate only
the numeric value of your response.