另一个潜在的优点,是飞机在跑道滑行时,机翼已经有一个较大的迎角。
Another potential advantage results from the fact that the plane is already tilted to a large Angle of attack as it rolls down the runway.
迎角,机翼翼弦在空气中向前运动时与自由气流之间的夹角。
Angle of ATTACK, the Angle of the wing chord in relation to the free stream airflow as it moves forward through the air.
考虑结冰对临界迎角、升阻特性等的影响,通过建立非线性动力学仿真模型和特殊情况下驾驶员操纵副翼偏转模型,实现了机翼结冰后的人-机系统动态仿真。
In order to quantitatively analyze the flight risk for wing icing, the probability assessment was proposed in which the simulation data of the pilot-aircraft-environment system was utilized.
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