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Fluidic Split Flap Systems for Yaw Control in Forward Flight
Fluidic Split Flap Systems for Yaw Control in Forward Flight
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机译:用于前向飞行中的偏航控制的流体分配翼片系统
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摘要
An active flow control system for generating yaw control moments for an aircraft during forward flight. The system includes right and left yaw effectors disposed proximate the right and left wingtips of the wing. A pressurized air system includes a pressurized air source and a plurality of injectors operably associated with the right and left yaw effectors that influence the path of airflow above and below the yaw effectors. Based upon which of the injectors is injecting pressurized air, the right and left yaw effectors generate no yaw control moment, generate a yaw right control moment or generate a yaw left control moment.
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