Release Time:2023-01-07 Hits:
Date of Publication: 2022-10-06
Journal: 中国宇航学会固体火箭推进专业委员会第三十届年会
Institution: 运载工程与力学学部
Note: 新增回溯数据
Prev One:A new device and method for simulating hypersonic aerothermal environment
Next One:硅基材料烧蚀模型的影响参数研究