Zobrazeno 1 - 1
of 1
pro vyhledávání: '"Xinguo Sha"'
Publikováno v:
Advances in Mechanical Engineering, Vol 15 (2023)
The boundary layer state has a critical effect on hypersonic vehicle performance and the noise level is the main factor causing the differences between the boundary layer transition in a wind tunnel test and that in a real flight. The second mode wav
Externí odkaz:
https://doaj.org/article/0855459e06984404b2f04a928d16cc6f
