(a) An airplane flies at constant speed along a

straight line at an angle of 30' with the
horizontal. The weight of the airplane is
80000 N and its engine provides a thrust of
100000 N in the direction of flight.
Determine the lift force perpendicular to the
airplane's wings and the force due to air
resistance opposite to the airplane's
direction of motion. Draw the free-body
diagram for the airplane. Identify the no-
work force from amongst the four forces
being exerted on the airplane.

1 answer

lift is not perpendicular to wings but perpendicular to the apparent air velocity (direction of motion ). You got it right about drag.

Is the plane following a horizontal path with nose tipped up 30 degrees (or 30 minutes, I can not tell from your text) or is it climbing or diving?

Since lift is perpendicular to the direction of motion, it does no work.