Progress in shock wave/boundary layer interactions
DV Gaitonde - Progress in Aerospace Sciences, 2015 - Elsevier
Recent advances in shock wave boundary layer interaction research are reviewed in four
areas:(i) understanding low frequency unsteadiness,(ii) heat transfer prediction …
areas:(i) understanding low frequency unsteadiness,(ii) heat transfer prediction …
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 …
shocks, which induces complex internal flows. This paper comprehensively reviews the …
Recent research progress on unstart mechanism, detection and control of hypersonic inlet
The present paper aims to provide a summary report on recent research progress about
unstart mechanism, detection and control of hypersonic inlet to help the researchers working …
unstart mechanism, detection and control of hypersonic inlet to help the researchers working …
Pseudo-shock waves and their interactions in high-speed intakes
F Gnani, H Zare-Behtash, K Kontis - Progress in Aerospace Sciences, 2016 - Elsevier
In an air-breathing engine the flow deceleration from supersonic to subsonic conditions
takes places inside the isolator through a gradual compression consisting of a series of …
takes places inside the isolator through a gradual compression consisting of a series of …
Unstart phenomena induced by flow choking in scramjet inlet-isolators
A review of recent research outcomes in downstream flow choking-driven unstart is
presented. Unstart is a flow phenomenon at the inlet that severely reduces the air mass flow …
presented. Unstart is a flow phenomenon at the inlet that severely reduces the air mass flow …
A review of the scramjet experimental data base
RK Seleznev, ST Surzhikov, JS Shang - Progress in Aerospace Sciences, 2019 - Elsevier
The frontier in hypersonic flights via an air-breathing scramjet faces a formidable challenge,
because the operational principle is built on thermal compression, which is inherently …
because the operational principle is built on thermal compression, which is inherently …
Exploiting active subspaces to quantify uncertainty in the numerical simulation of the HyShot II scramjet
PG Constantine, M Emory, J Larsson… - Journal of Computational …, 2015 - Elsevier
We present a computational analysis of the reactive flow in a hypersonic scramjet engine
with focus on effects of uncertainties in the operating conditions. We employ a novel …
with focus on effects of uncertainties in the operating conditions. We employ a novel …
Ram-scram transition and flame/shock-train interactions in a model scramjet experiment
ML Fotia, JF Driscoll - Journal of Propulsion and Power, 2013 - arc.aiaa.org
The behavior of a ram-scram transition was examined using a direct-connect model scramjet
experiment along with pressure measurements and high-speed laser interferometry. The …
experiment along with pressure measurements and high-speed laser interferometry. The …
Low-frequency unsteadiness of shock-wave/boundary-layer interaction in an isolator with background waves
Z Wang, J Chang, W Hou, D Yu - Physics of Fluids, 2020 - pubs.aip.org
Low-frequency unsteadiness is investigated through wind tunnel experiments and numerical
simulations of the internal flow in a supersonic isolator with background waves generated by …
simulations of the internal flow in a supersonic isolator with background waves generated by …
Experimental investigation of unstart dynamics driven by subsonic spillage in a hypersonic scramjet intake at Mach 6
Understanding start–unstart behavior of intakes in hypersonic Mach numbers is essential for
seamless operation of scramjet engines. We consider a high compression ratio intake (CR …
seamless operation of scramjet engines. We consider a high compression ratio intake (CR …