CAJ | 학술논문

本文采用非结构网格和标准k-epsilon（2eqn）模型，建立相应的控制方程对NACA0012机翼进行求解，得到了机翼的升力系数、升阻比随近地（海）距离变化曲线及拟合函数。采用非结构网格和标准k-epsilon（2eqn）模型和滑移网格、动边界模拟近地爆炸冲击波对近地飞行器压力的影响，得到了在该试验条件下受力随时间的变化趋势曲线。本文结果可以为研究地效飞行器近地飞行时气动性能分析及遇到爆炸等不稳定的近地（海）条件下飞行器的平稳性、安全性设计提供一些理论上的支持。
본문채용비결구망격화표준k-epsilon（2eqn）모형，건립상응적공제방정대NACA0012궤익진행구해，득도료궤익적승력계수、승조비수근지（해）거리변화곡선급의합함수。채용비결구망격화표준k-epsilon（2eqn）모형화활이망격、동변계모의근지폭작충격파대근지비행기압력적영향，득도료재해시험조건하수력수시간적변화추세곡선。본문결과가이위연구지효비행기근지비행시기동성능분석급우도폭작등불은정적근지（해）조건하비행기적평은성、안전성설계제공일사이론상적지지。
In this paper,unstructured grids and standard k-epsilon(2eqn) model,to establish the appropriate equations to solve for NACA0012 wing, got the lift coefficient of the wing,the lift-drag ratio with(sea) from the curve of the near-Earth and the fitting function.Unstructured grids and standard k-epsilon(2eqn) model and the sliding mesh,dynamic simulation of near-Earth boundary blast pressure effects on near-Earth spacecraft,has been in force under the test conditions change with time trend curves.Our results may be flying under the aerodynamic performance analysis and experiencing explosions near the unstable ground(sea) condition of the aircraft stability,security,designed to provide some theoretical support for the study of near-Earth ground effect vehicles.