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METHOD FOR ENHANCING THE AERODYNAMIC EFFICIENCY OF THE VERTICAL TAIL OF AN AIRCRAFT
METHOD FOR ENHANCING THE AERODYNAMIC EFFICIENCY OF THE VERTICAL TAIL OF AN AIRCRAFT
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机译:飞机垂直尾翼气动性能的方法
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摘要
The invention comprises varying the ratio between the control surface local chord (I) and the vertical stabilizer local chord (L) along the height of the vertical tail (2) in order to adapt the local value of the coefficient of the side lift applied to the vertical tail (2) to a maximum acceptable value of the side lift coefficient.
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