首页> 美国政府科技报告 >LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION HAVING SPLIT FLAPS LOCATED AHEAD OF THE WING TRAILING EDGE AND LEADING- AND TRAILING-EDGE FLAPS ON THE CANARD CONTROL
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LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION HAVING SPLIT FLAPS LOCATED AHEAD OF THE WING TRAILING EDGE AND LEADING- AND TRAILING-EDGE FLAPS ON THE CANARD CONTROL

机译:具有分叉翼片的CaNaD飞机配置的低速气动特性位于翼形边缘上方和牵引带和牵引边缘翼上的CaNNa控制

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摘要

Canard aircraft with split flaps ahead of the wing trailing edge and flaps on the leading and trailing edges of the canard control at low speed

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