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ELEVON DESIGN FOR ALL-AXIS CONTROL IN A BLENDED WING BODY AIRCRAFT
ELEVON DESIGN FOR ALL-AXIS CONTROL IN A BLENDED WING BODY AIRCRAFT
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机译:混合机翼飞机全轴控制的提升设计
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摘要
Technologies for providing blended wing body aircraft control surfaces are described herein. In some examples, one or more of the control surfaces have angular configurations that reduce the formation of air vortexes when in upward or downward configurations, thereby reducing the drag on the aircraft when the control surfaces are being used.
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