10. (35) An aircraft is in steady level flight at 8000 meters altitude (standard conditions for this altitude) with a velocity of 150 . The jet engines it uses have a bypass ratio m S mfan (2: of 8 and a total inlet area of 5 square meters for both engines combined. mcore/ The air is accelerated by 50 meters per second before entering the inlets of the engines. The flow through the core of each engine is accelerated to Mach 1.1 (using the reference temperature given above). The flow through the fan is accelerated to 290 " but thrust reversers are deployed, redirecting only the fan flow 90 degrees m S (perpendicular to the axis of the engine). How much thrust is the aircraft generating along the axis of the engine? (Image below for visualization aid, all pertinent details in the text of the problem) Reversers Not Deployed Reversers Deployed Blue= Flow through the fan, core flow not shown