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

H Huang, H Tan, F Li, X Tang, Y Qin, LB Xie… - Progress in Aerospace …, 2023 - Elsevier
A hypersonic inlet/isolator acts as the “compressor” for scramjet engines through a series of
shocks, which induces complex internal flows. This paper comprehensively reviews the …

[HTML][HTML] A review of three-dimensional shock wave–boundary-layer interactions

K Sabnis, H Babinsky - Progress in Aerospace Sciences, 2023 - Elsevier
The vast majority of shock wave–boundary-layer interactions in practical applications like
supersonic aircraft intakes are three dimensional in nature. The complex behaviour of such …

Numerical study of a scramjet isolator performance under different sidewall compression angles

JVMB de Siqueira, GB Ribeiro - Thermal Science and Engineering …, 2023 - Elsevier
Scramjet engines, also known as supersonic combustion ramjet engines, are frequently
regarded as a compelling alternative for launching payloads into Earth's orbit. These air …

Identification of discrete tonal noise in inclined jet impingement using pressure-sensitive paint

X Liu, C Qin, K Zhao, P Wang, Y Liu, D Peng - AIAA Journal, 2023 - arc.aiaa.org
This paper presents the utilization of fast-responding pressure-sensitive paint (fast PSP) to
identify the discrete tonal noise generated in 55 deg inclined jet impingement. Cases of …

Low-frequency large-scale unsteadiness analysis of lateral jet interactions on a slender cylinder in hypersonic flows using fast-responding pressure-sensitive paint

X Liu, J Zhong, Z Dong, X Fan, D Zou, Y Liu… - … Thermal and Fluid …, 2024 - Elsevier
Lateral jet interactions, commonly encountered in high-speed vehicles, are typical complex
three-dimensional (3D) shock wave/boundary layer interactions. The spatiotemporal …

Experimental characterization of shock-separation interaction over wavy-shaped geometries through feature analysis

J Braun, I Rahbari, G Paniagua, P Aye-Addo… - … Thermal and Fluid …, 2024 - Elsevier
A canonical wavy surface exposed to a Mach 2 flow is investigated through high-frequency
Pressure Sensitive Paint, Kulite measurements, and shadowgraph imaging. The wavy …

Spanwise unsteadiness in the sidewall-confined shock-wave/boundary-layer interaction

X Liu, L Chen, Y Zhang, H Tan, Y Liu… - Journal of Fluid …, 2024 - cambridge.org
Three-dimensional effects of sidewalls on the low-frequency unsteadiness of the shock-
wave/boundary-layer interaction (SBLI) are of academic and practical importance but not yet …

[HTML][HTML] Experimental and numerical simulation of the attenuation effect of blast shock waves in tunnels at different altitudes

C Liu, H Li, Z Wang, Y He, G Zhang, M Wang - Defence Technology, 2025 - Elsevier
Traffic engineering such as tunnels in various altitudinal gradient zone are at risk of
accidental explosion, which can damage personnel and equipment. Accurate prediction of …

[HTML][HTML] On space–time diversity in shock train self-excited oscillation mode during wide-range evolution in a scramjet isolator

Y Ji, M He, X Huang, H Sheng, W Wang, M Xie, H Liu - AIP Advances, 2024 - pubs.aip.org
The shock train self-excited oscillation can induce combustor instabilities and reduce engine
margin. In a dual-mode scramjet, the shock train undergoes a complete evolution process …

Effects of Surface Roughness on Shock-Wave/Boundary-Layer Interactions at Mach 7.2

ENA Hoffman - 2023 - search.proquest.com
This research work studies the effects of surface roughness on shock-wave/boundary-layer
interactions (SWBLIs). SWBLI are prevalent in supersonic and hypersonic flows and occur …