1) pitching characteristic
俯仰特性
2) pitching moment characteristic
俯仰力矩特性
1.
When angle of attack is changing from-10° to 7°,the effects of viscosity on the lift,drag force and pitching moment characteristics of hypersonic vehicle in three working conditions including inlet closed,inlet open but unfired,inlet open and fired were discussed.
采用二维耦合隐式NS方程和标准k-ε湍流模型对高超声速飞行器在进气道关闭、发动机通流以及发动机点火工作状态下的内外流场进行了数值仿真研究,离散采用二阶迎风格式,分析了在不同攻角(-10°~7°)条件下,粘性对处于三种不同的工作状态下高超声速飞行器升力特性、阻力特性以及俯仰力矩特性的影响。
2.
Two-dimension coupled implicit Naviers-Stokes equations and standard k-ε viscid models were introduced to simulate the lift characteristic,drag characteristic,pitching moment characteristic and lift-to-drag ratio characteristic of integrated hypersonic vehicle with Hark head configuration working under the conditions of inlet closed,inlet open but unfired and inlet open and fired.
采用二维耦合隐式N-S(Navier-Stokes)方程和标准k-ε湍流模型对具有哈克外形头部的一体化高超声速飞行器在进气道关闭、发动机通流以及发动机点火状态下的升力特性、阻力特性、俯仰力矩特性以及升阻比特性进行了数值模拟,考察了机身头部长细比对其气动性能的影响,结果发现,在第一种定义方式下的飞行器构型气动性能改良程度明显高于第二种定义方式,同时,随着机身头部长细比的增加,一体化高超声速飞行器的气动性能得到明显提高,可以满足飞行器巡航时的气动要求。
3) pitch agility
俯仰敏捷性
1.
In this paper, effects of horizontal tail volume coefficient on the pitch agility metrics are discussed through comparison computations.
研究了平尾尾容系数对飞机俯仰敏捷性尺度的影响。
4) longitudinal control; fore-and-aft control
俯仰操纵性
5) pitching stability
俯仰稳定性
6) pitch
[英][pɪtʃ] [美][pɪtʃ]
俯仰
1.
The coupling dynamics of the pitching of spacecraft, the sloshing of liquid fuel and the vibration of elastic appendages are investigated.
该文考虑了带弹性帆板与液体燃料的航天器做俯仰运动时刚-液-弹之间的相互耦合作用,采用已推导的刚-液-弹耦合系统非线性动力学方程组,应用多尺度法解析分析耦合系统的液体一阶主共振,利用奇异性理论对分岔方程进行分析,得到多种分岔模式,随后根据该文研究的耦合系统物理系数范围,确定只存在滞后点分岔,表现为幅频曲线软、硬特性的转换现象。
2.
The coupled dynamics of the pitching of a spacecraft,the sloshing of liquid fuel and the vibration of elastic appendages is investigated.
考虑了带弹性帆板与液体燃料的航天器做俯仰运动时刚-液-弹之间的相互耦合作用,采用已推导的刚-液-弹耦合系统非线性动力学方程组,应用多尺度法对耦合系统液体一阶主共振的非线性动力学特性进行解析分析,发现了幅频曲线软、硬特性随液深发生转换的现象,发生转换时的临界液深值大小与液体燃料在航天器中的位置、航天器与弹性帆板的转动惯量相对于液体燃料密度的比值均有关,并通过与数值模拟比较,验证了解析分析的正确性。
3.
The effects of fuel position on the attitude of spacecraft with elastic appendages were studied under the condition that the fuel sloshes violently and assuming that the coupling system pitches round the mass center of the whole system.
假设耦合系统绕系统质心做俯仰运动,首先采用已推导的刚-液-弹耦合系统俯仰运动非线性动力学方程组,得到系统固有频率,给出固有频率简单近似解析表达式,分析充液箱位置对系统各阶固有频率的影响。
补充资料：俯仰
〈书〉①低头和抬头：～之间。②指一举一动：～由人。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条