level flight造句
例句与造句
- The same considerations apply to the correct banking angle of a plane when it makes a turn in level flight .
当水平飞行的飞机转弯时，同样应有一定的倾斜，倾斜角的大小可按与上面相同的考虑来决定。 - Okay , adjust for the wind . nice , level flight
好，适应一下风向不错，平飞 - Okay , adjust for the wind . nice , level flight
好，适应一下风向不错，平飞 - The aircraft is lost control now , i can not maintain level flight at present altitude
飞机现在失去操纵，我在现在的高度上不能保持平飞。 - We will stop dumping for the time being , the dumping must be carried out at straight level flight
我们将暂时停止放油，放油必须要一直平飞。 - It's difficult to find level flight in a sentence. 用level flight造句挺难的
- From straight and level flight , after the helicopter passes the pilot , execute a 180 degree turn away from the pilot
先保持水平直线飞行，当直升机通过操控者后，开始执行外侧180转弯的动作（远离操控者） 。 - Starting from straight and level flight after the helicopter passes the pilot , the helicopter is smoothly pulled vertical ( aft cyclic )
先保持水平直线飞行，当直升机通过操控者后，开始平滑地拉高机头（打升舵） ，使机头朝上垂直爬升。 - Starting from straight and level flight after the helicopter passes the pilot , the helicopter is smoothly pulled through a loop ( aft cyclic )
先保持水平直线飞行，当直升机通过操控者后，开始平滑地拉高机头（打升舵） ，使飞行轨迹成为一个环状。 - The helicopter is allowed to fall the same distance that it climbed at the beginning of the maneuver before pulling the helicopter back to straight and level flight
待直升机垂直俯冲的距离与垂直爬升的距离相同时，拉起机头恢复成水平直线飞行。 - Based on the mathematical model developed by the paper , the trim calculations are carried out in the conditions that the example aircraft converts from helicopter to airplane mode in level flight with zero longitudinal acceleration and angular rate
本文依据所建立的样例机纵向动力学模型,假定飞机在给定高度平飞,纵向加速度和角加速度均为零,完成过渡模式下的动力学配平。 - According to purpose of the towed flight , a new trajectory consisting of taking off , climbing phase , level flight phase is presented with . trajectory pitch angle of the towing plane is optimized . according to the flight law of the towing plane , the fin deflection angle and amplification coefficient of particle - system trajectory of carrier rocket are designed , in order to realizing flight steadily of the carrier rocker
根据牵引飞行的目的，对载机应用了“起飞?爬升?平飞”的变轨道飞行方案，同时对载机轨道的倾角、倾角变化规律进行优选设计；再根据载机的飞行规律，对运载器质点系轨道的舵偏规律及其放大系数进行了设计计算，实现运载器稳定牵引飞行。