Transient Flow Evolution of a Hypersonic Inlet/Isolator with Incoming Windshear

Transient Flow Evolution of a Hypersonic Inlet/Isolator with Incoming Windshear

In this paper, a novel flow perturbation model meant to investigate the effects of incoming wind shear on a hypersonic inlet/isolator is presented. This research focuses on the transient shock/boundary layer interaction and shock train flow evolution in a hypersonic inlet/isolator with an on-design...

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Bibliographic Details
Main Authors: Simin Gao, Hexia Huang, Yupeng Meng, Huijun Tan, Mengying Liu, Kun Guo
Format: Article
Language:English
Published: MDPI AG 2023-12-01
Series:Aerospace
Subjects:
wind shear
hypersonic inlet/isolator
shock wave/boundary layer interaction
shock train
unsteady simulation
Online Access:https://www.mdpi.com/2226-4310/10/12/1021

Internet

https://www.mdpi.com/2226-4310/10/12/1021

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