Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Songxiang Tang"'
Publikováno v:
Applied Sciences, Vol 14, Iss 22, p 10234 (2024)
A transonic hump with a Mach number (M∞) of 0.875 was utilized to compare the prediction capabilities of RANS, URANS, IDDES, and IDDES-SLA for shock-induced separation. The results matched the experimental data concerning pressure, friction coeffic
Externí odkaz:
https://doaj.org/article/1ca79892f6224a77aa67f4af79fcbe13
Publikováno v:
Aerospace, Vol 9, Iss 10, p 567 (2022)
Flow separation is easily induced at the junctions of aircraft components, and for aircraft with T-type tails, in particular, it can lead to loss of directional stability under a small sideslip angle. In the reported study, improved delayed detached
Externí odkaz:
https://doaj.org/article/8c75bdb202584b189b6df0098c851100
Publikováno v:
International Journal of Computational Fluid Dynamics. 36:731-751
Publikováno v:
International Journal of Computational Fluid Dynamics. 36:404-423