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Numerical research on the propagation characteristics and evolution mechanisms of rotating detonation waves with the spatial fluctuation of inlet total pressure

The Physics of Fluids
The stable combustion of rotating detonation engines is significantly affected by inlet spatial fluctuation, especially during aircraft maneuvering, necessitating extensive research for further engineering enhancements.
Xiangjun Zhang   +6 more
semanticscholar   +1 more source

Formation of detonation in rotating channels

Doklady Physics, 2010
308 For estimating the possibility of detonation initia tion during rotation, we considered the gasmixture flow inside and outside the rotating elliptic cylinder included in the circular cylinder. The values of critical parameters at which the detonation is formed were determined.
V. A. Levin   +2 more
openaire   +1 more source

Analysis of waves dynamics in a rotating detonation combustor fueled by kerosene

The Physics of Fluids
The wave dynamics play a crucial role in the operation characteristics of the rotating detonation engine. We conducted numerical simulations of a rotating detonation combustor (RDC) using multicomponent reactive Navier–Stokes equations coupled with a ...
Wenqi Fan   +5 more
semanticscholar   +1 more source

Numerical Investigation of Rotating Detonation Engines

46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2010
Rotating detonation engines (RDE’s) represent an alternative to the extensively studied pulse detonation engines (PDE’s) for obtaining propulsion from the high efficiency detonation cycle. Since it has received considerably less attention, the general flow-field and effect of parameters such as stagnation conditions, combustion chamber length, and fuel
Douglas Schwer, Kailas Kailasanath
openaire   +1 more source

Performance Characterization of a Radial Rotating Detonation Combustor with Axial Exhaust

Journal of Engineering For Gas Turbines and Power
This experimental study characterizes the performance of a radial rotating detonation combustor (RDC). An aerospike nozzle for rocket propulsion has been integrated into the center of the combustor, although the same combustor could also be coupled ...
Dalton G. Langner   +3 more
semanticscholar   +1 more source

LES Investigation of Film Cooling in Rotating Detonation Combustors

Heat Transfer
High-power density combustors like Rotating Detonation Combustors (RDC) offer significant benefits. However, they must overcome many challenges to be integrated into a gas turbine.
Shreyas Ramanagar Sridhara   +3 more
semanticscholar   +1 more source

Rocket rotating detonation engine flight demonstrator

Aircraft Engineering and Aerospace Technology, 2016
Purpose Today’s modern liquid propellant rocket engines have a very complicated structure. They cannot be arbitrarily downsized, ensuring efficient propellants’ mixing and combustion. Moreover, the thermodynamic cycle’s efficiency is relatively low.
Adam Okninski   +2 more
openaire   +1 more source

Analytical study of rotating detonation and engine operating conditions

The Physics of Fluids
In this paper, the mechanism of rotating detonation is analytically discussed using a two-dimensional sheet model. Two ratios are employed in this discussion: the ratio of the sonic point width to the detonation front width, and the ratio of the ...
Takeshi Kanda, Hidetaka Inagaki
semanticscholar   +1 more source

Numerical simulations and theoretical analysis of the forward shock wave in a non-premixed air-breathing rotating detonation combustor

The Physics of Fluids
The forward shock wave induced by the detonation wave propagates in the inlet and restrains the air from being injected into the rotating detonation engine, and the stable continuous propagation of the detonation wave is affected.
Sijia Gao   +4 more
semanticscholar   +1 more source

An experimental study on gas-solid two-phase rotating detonation ramjet engine based on aluminum powder fuel

Journal of Physics: Conference Series
In order to explore the feasibility of solid powder detonation technology, the ground direct connection test of aluminum powder/hydrogen/air fuel detonation engine was carried out in this paper.
Jianing Jing, Hu Ma
semanticscholar   +1 more source

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