00:00During high-speed turns, the F-135 engine adjusts its nozzle to prevent airflow disruption.
00:06Centrifugal forces distort inlet pressure profiles, compelling actuator rings to dynamically alter throat geometry.
00:13Rapid directional acceleration forces complex shockwave patterns to migrate across the supersonic inlet ramp.
00:21Advanced control systems dynamically adjust the exhaust nozzle area, optimizing bypass flow to maintain stall-free engine operation.
00:30The variable area fan nozzle adjusts airflow to prevent compressor stall at supersonic speeds.
00:35Any age, any background, same opportunity, sell, earn, repeat.
00:41Join our marketing team.
