Write a function to calculate the contribution of each major component of the engine shown in the figure below to the production of the total engine thrust. The pictured engine is a Rolls Royce engine, and you have the area $(),$ pressure different $(),$ and velocity $()$ at the exit of each component. You are also provided the mass flow of air through the engine.

function T $=$ thrustcalcs$($Ae$,$ dp$,$ Ve$,$ m$\_$dot$)$