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)
