A review of the shock-dominated flow in a hypersonic inlet/isolator-Reference-Cited by-全球学者库

A review of the shock-dominated flow in a hypersonic inlet/isolator

Published:2023-11 Issue: Volume:143 Page:100952
ISSN:0376-0421
Container-title:Progress in Aerospace Sciences
language:en
Short-container-title:Progress in Aerospace Sciences

Author:

Huang He-xia^ORCID,Tan Hui-jun,Li Fang-bo^ORCID,Tang Xue-bin,Qin Yuan,Xie Li-Bin^ORCID,Xu Yao-Yu,Li Can-min,Gao Si-min,Zhang Yue,Sun Shu,Zhao Dan^ORCID

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference262 articles.

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5. Experimental investigation of the starting behavior of a three-dimensional scramjet intake;Flock;AIAA J.,2015

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2. On low-frequency unsteadiness of single-incident and dual-incident shock waves/turbulent boundary layer interactions with large-scale separations;Physics of Fluids;2024-01-01

3. Generalized prediction for self-starting performance of two-dimensional hypersonic inlets;Physics of Fluids;2024-01-01

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