1.
moment due to elevator deflection
偏转升降舵产生的力矩
2.
Repeat push forward cyclic completing a minimum of two (2) forward tumbles.
将升降舵打降舵，重覆步骤3，向前翻滚至少二圈。
3.
the horizontal stabilizer and elevator in the tail assembly of an aircraft.
飞机尾部的水平稳定器和升降舵。
4.
A control surface on an airplane that combines the functions of an elevator and an aileron.
升降副翼兼有升降舵和副翼两种功能的飞机控制平面
5.
With the helicopter upright and flying backward straight and level from the left to the right, when the helicopter is directly in front of the pilot, push forward cyclic and execute a Tail first Inside Loop.
由左至右保持后退水平直线飞行，当直升机在操控者的正前方时，将升降舵打降舵执行内觔斗。
6.
the horizontal surface of an aircraft's tail assembly that is fixed and to which the elevator is hinged.
固定的连着升降舵的在飞机尾部的水平面。
7.
a lever used by a pilot to control the ailerons and elevators of an airplane.
飞行员用来控制飞机升降舵和副翼的杠杆。
8.
A variable pitching moment is provided by moving the elevator.
俯仰力矩的变化由升降舵的偏转来提供。
9.
Research of Calibration Technology on Angular Displacement for Elevator, Aileron and Flap of Airplane;
飞机升降舵、副翼和襟翼转角标定技术研究
10.
Test and analysis on load bearing capability of hinge lug of aircraft horizontal stabilizer elevator
飞机平尾升降舵接头耳片承载能力分析与试验
11.
Design and Realization of the Submarine Elevator Automatic Control Based on VSS
基于VSS的潜艇升降舵自动控制设计与实现
12.
With the helicopter hovering Tail-In pull back cyclic, and work the collective to complete at least two (2) full back tumbles while maintaining a constant altitude and heading.
机尾朝向操控者保持停悬，将升降舵拉升舵使直升机保持固定的高度及方向，向后翻滚至少二圈。
13.
With the helicopter hovering Nose-In pull back cyclic, and work the collective to complete at least two (2) full back tumbles while maintaining a constant altitude and heading.
机头朝向操控者保持停悬，将升降舵拉升舵使直升机保持固定的高度及方向，向后翻滚至少二圈。
14.
Repeat the above steps, but use aft cyclic instead of forward cyclic completeing at least three(3)" backward" tumbles.
重覆执行上述步骤，但将升降舵打降舵，至少须完成三次后滚翻的动作。
15.
Evidence from the flight data recorder indicates the elevators were set at a wrong angle for landing.
飞行资料记录器显示在降落的时候升降舵的角度设置错误
16.
The rudder hinge moment and control force are treated in a manner similar to that employed for the elevator.
研究方向舵铰链力矩和操纵力的方法与研究升降舵所采用的方法相似。
17.
In mode2, the right control stick operates the aileron and elevator and the left stick operates the rudder and throttle.
在模式2中，右边的操纵杆控制副翼和升降舵，左边的操纵杆控制方向舵和油门。
18.
We have trouble with elevator control, it is fluttering( sharking) slightly, we're to keep higher approach speed on final.
升降舵操纵系统故障，轻微抖动，我们在五边保持稍大进场速度。