对称着陆 meaning in English
symmetrical landing
Examples
- Finally , the author analyzed the results of the dynamic simulation and given a rough conclusion about the distribution of the ground loads of the aircraft researched among its different landing gears
对仿真结果进行对比分析,定性地给出该飞机在对称着陆过程中飞机所受地面载荷在各个起落架缓冲支柱上的分布关系。 - It is proved by the analysis that , during the symmetric landing of that airplane , the impact load of the after main landing gear is the largest among those landing gears and the nose landing gear comprised of about 18 percent of the total impact load
分析表明:该样机在对称着陆过程中,后主起落架承受的地面载荷最大,前起落架轮胎仅承担了全机18 %的冲击载荷,载荷分布较普通的前三点式起落架有明显的改善。 - At last , the researchers discussed and analyzed the results of the simulation contrastively . firstly , according to the conditions of the aircraft being researched , differential coefficient equations of the aircraft during its symmetric landing are established systemically in this paper
文章的主要内容包括:以某多轮多支柱飞机的起落架为例,依据该起落对称着陆的实际情况,系统地建立了该飞机的全机着陆动力模型以及飞机主起落架数学模型。 - Now , it is worthwhile to conduct the research on the ground load of landing gear with multi - wheels and multi - struts according to the basic theories of the mechanics , the dynamics analysis model of the full - aircraft during its landing process is established in this paper
本文首先以某多轮多支柱飞机的起落架作为研究对象,应用动力学基本原理,建立了全机的着陆动力学模型。然后,通过利用大型动力学仿真软件adams对该飞机进行了对称着陆仿真,并对仿真结果进行了对比分析。 - Secondly , a full - aircraft assembly model in software adam is defined , which includes an airframe subsystem , a strut subsystem of the nose landing gear , a wheel subsystem of the nose landing gear , a strut subsystem of the forward main landing gear , a wheel subsystem of the forward main landing gear , a strut subsystem of the after main landing gear and a wheel subsystem of the after main landing gear
在adams软件中建立了一个由机身、前起落架缓冲支柱、前起落架机轮、前主起落架缓冲支柱、前主起落架机轮、后主起落架缓冲支柱和后主起落架机轮七个子系统构成的全机模型,并对该模型进行了对称着陆仿真分析。