Investigation of hydrogen-enriched kerosene-fueled rotating detonation engine with multi-column film cooling

J Li, J Yu, J Li, Y Lei, S Yao, W Zhang - Physics of Fluids, 2024 - pubs.aip.org
To address the thermal protection challenges associated with the rotating detonation engine
(RDE) in engineering applications, this study employs a three-dimensional numerical …

Analysis of coupling supersonic turbine stage with rotating detonation combustor under different turbine parameters

L Su, F Wen - Aerospace Science and Technology, 2024 - Elsevier
The rotating detonation gas turbine boasts several advantageous characteristics, including
self-pressurization, minimal entropy increase, high thermal efficiency, and a high thrust-to …

Reduced-order-modeling of the transient starting in supersonic passages

LB Inhestern, D Peitsch, G Paniagua - Aerospace Science and Technology, 2023 - Elsevier
Characterizing the time scales of starting in supersonic passages is essential for future
aerospace propulsion systems, such as supersonic intakes, Rotating Detonation Engines …

Influence of oncoming flow parameters on rotating detonation combustor with supersonic turbine guide vanes

F Wen, L Su, Y Wang, J Han, S Wang - Physics of Fluids, 2024 - pubs.aip.org
Rotating detonation combustion can greatly improve the performance of air-breathing
turbojet engines due to its self-pressurization and high combustion efficiency. Detonation …

Numerical Optimization of a Reacting Radial Rotating Detonation Engine using Cross-Sectional Area Profiling

K Bell, AK Agrawal - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
Most previous and current rotating detonation combustion (RDC) research has focused on
annular RDCs, in which reactants are injected axially, and the exhaust flow is predominantly …