Characterizations of Swept Shock/Boundary Layer Interactions: A Comparison Between Planar Shock, Curved Shock, and Isentropic Compression

To investigate the flow characteristics of three-dimensional swept interactions, 3D steady Reynolds-averaged Navier–Stokes (RANS) simulations are conducted at an incoming Mach number of 3.5 and a Reynolds number of 30,955 based on the incoming boundary-layer thickness <i>δ</i>₀. Three ind...

Whakaahuatanga katoa

Ngā taipitopito rārangi puna kōrero

Ngā kaituhi matua:	Fajia Sheng, Dengxue Song, Hexia Huang, Huijun Tan, Xiankai Li, Zhiyu Zhang
Hōputu:	Artigo
Reo:	Inglês
I whakaputaina:	MDPI AG 2026-06-01
Rangatū:	Aerospace
Ngā marau:	three-dimensional swept interactions quasi-conical similarity primary vortices compression efficiency mass flow capture
Urunga tuihono:	https://www.mdpi.com/2226-4310/13/6/539
Ngā Tūtohu:	Tāpirihia he Tūtohu Kāore He Tūtohu, Me noho koe te mea tuatahi ki te tūtohu i tēnei pūkete!