CAJ | 학술논문

本文使用ansys fluent对二维机翼在近地（海）条件下受力分析，得出了飞行器在近地（海）状况变化不大条件下飞行器的受力分布、周围流体场的分布和在飞行器附近存在爆炸压力波情况下飞行器受力变化以及周围流体场的变化情况，可以为研究地效飞行器的研究人员在研究地效飞行器遇到爆炸等不稳定的近地（海）条件下飞行器额平稳性操作，平稳性设计提供一些理论上的基础。
본문사용ansys fluent대이유궤익재근지（해）조건하수력분석，득출료비행기재근지（해）상황변화불대조건하비행기적수력분포、주위류체장적분포화재비행기부근존재폭작압력파정황하비행기수력변화이급주위류체장적변화정황，가이위연구지효비행기적연구인원재연구지효비행기우도폭작등불은정적근지（해）조건하비행기액평은성조작，평은성설계제공일사이론상적기출。
This paper used ansys fluent to make stress analysis to the II dimension wing in near-Earth (sea) conditions and got that the force distribution and the distribution of around fluid field under the situations with little change of near-Earth (sea) conditions and the force changes and the changes situation of around fluid field when existed explosion pressure wave situation around the aircraft, which could provide some theoretical basis for the research personnel studying the smooth operation and design of the ground effect vehicles when it encountered explosion and other unstable situations.