1) airplane load
飞机荷载
1.
A mechanical model of the complicated coupling system , composed of airplane load, runway and foundation, was introduced.
本文首先介绍了飞机荷载—道面—地基复杂耦合系统的力学模型,然后针对机场战时抢修的实际问题,对折叠式玻璃钢道面板系统的若干典型工况进行了有限元数值分析,计算结果将为折叠式玻璃钢道面板系统的设计提供依据。
2) aircraft ground load
飞机地面载荷
1.
Application of virtual prototyping technology in the analysis of aircraft ground load
虚拟样机技术在飞机地面载荷分析中的应用
3) Aircraft loads monitoring
飞机载荷监控
4) flight loads
飞行载荷
1.
A method synchronously computing longitudinal maneuvering flight and flight loads based on nonlinear wind-tunnel test aerodynamic forces(experimental aerodynamic forces for short)was proposed.
提出了一种基于非线性风洞试验数据(简称试验气动力)同步进行纵向机动飞行过程和飞行载荷的计算分析方法。
5) flight load
飞行载荷
1.
Calculation method of flight load for military aircraft;
军用飞机飞行载荷计算方法研究
2.
According to the requirment of Military Aircraft Strenth and Rigidity Specification, the flight loads calculation methods and results by taking a fighter as an example have been introduced in this paper, considering aircraft construction flexibility, nonlinear aerodynamic characteristics and aerodynamic load distribution.
以某歼击机为例,按《军用飞机强度和刚度规范》要求,重点介绍了考虑飞机结构柔性和非线性气动力特性、气动载荷分布的飞行载荷计算方法和计算结果,并对柔性飞机的非线性气动力特性和气动载荷分布对飞行载荷计算状态和严重载荷设计情况选取的影响进行了对比和分析,确定了飞机严重载荷设计情况和设计载荷,从而得出一些具有实际工程参考价值的结论。
3.
Based on the equations of motion of flexible air vehicles including rigid-body modes and elastic structural modes, and applying influence coefficients of linear aerodynamics, a set of equations are derived and a method is presented for analysis of flight loads and dynamic characteristics.
在综合考虑了刚体运动自由度和弹性自由度的弹性飞行器运动方程的基础上 ,采用了线性气动力的影响系数形式 ,提出了一套飞行载荷与动态特性分析的方程和方法 ,用于解决飞行力学和气动弹性力学中的静气动弹性发散、配平与结构变形、气动载荷分布、颤振与飞行动态特性等问题。
6) flywheel load
飞轮载荷
补充资料：变后掠翼飞机(见后掠翼飞机)
变后掠翼飞机(见后掠翼飞机)
swing-wing aircraft
bianhoul位eyi feiii变后掠翼飞机(swing一wing aircran)见后掠翼飞机。
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