To enable the coupling of the unsteady, high-enthalpy flow exiting a Rotating Detonation Combustor (RDC) with a subsonic turbine, an ejector may be installed between the …
D Kim, M Asli, K Höschler - Aerospace, 2023 - mdpi.com
As the issue of pollutant emissions from aviation propulsion escalates, research into alternative powertrains is gaining momentum. Two promising technologies are the Hybrid …
To facilitate the integration of a rotating detonation combustor (RDC) in a turbomachine, adding an ejector downstream of the combustor may be a viable option. The present work …
The rotating detonation combustor is investigated as a potential implementation of pressure- gain combustion. Achieving net pressure-gain has proven to be extremely challenging in …
AD Feleo, M Gamba - AIAA Journal, 2024 - arc.aiaa.org
ROTATING detonation engines/combustors (RDEs/RDCs) are attractive technologies for the potential gain in thermodynamic efficiency. By nature of the continuously propagating …
View Video Presentation: https://doi. org/10.2514/6.2023-1292. vid A time resolved, two- dimensional reactive Euler solver is employed to simulate Rotating Detonation Combustion …
To generate favorable flow characteristics for turbine integration at the outlet of a Rotating Detonation Combustor (RDC), installing an ejector or bypass flow device between both …
Despite a global shift towards renewable energy sources, gas turbines are likely to continue playing an important role. However, a large part of their future fuel must be synthesized from …
Detonation-based combustors are attractive for potential increases in thermodynamic efficiency, leading to improved thrust or work production. Fundamentally, a detonation …