What is the maximum angle of climb (steady velocity climb) for a
turbojet powered aircraft with...
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Physics
What is the maximum angle of climb (steady velocity climb) for aturbojet powered aircraft with an (L?D)max equal to 10.5 and agross weight of 8000 lb. if it is producing a thrust of 2000 lb.?If the aircraft using the same available thrust, wishes toestablish a rate of climb equal to 1800fpm, what airspeed will itneed to establish? (Assume the required thrust equals764pounds)
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We consider that the velocity is steady and there is no acceleration We will use T for Thrust W for weight mg L for lift force D for Drag and for angle of climb T D W sin
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