iboyX5JNjO4ug0ayRCuelptMFryPSYdh2Hrgyjb4iTzRGY3q2sRXgEjh7SwF
Current position: Home >> Scientific Research >> Research Projects

高超声速飞行器颤振模型热响应的物理模拟方法

Release Time:2023-11-07  Hits:

Leading Scientist:孙士勇

Project Source:企事业单位委托科技项目

Status:在研

Supported by:Beijing Near Space Aircraft System Engineering Research Institute

Nature of Project:横向

Date of Project Approval:2017-08-01

Scheduled Completion Time:2019-03-01

Date of Project Initiation:2017-08-01

Prev One:高速全机静气动弹性风洞试验模型加工

Next One:智能抛物面天线在轨调节地面系统搭建与验证