Mass flow rate effect on a rotating detonation combustor with an axial air injection

T Sato, F Chacon, M Gamba, V Raman - Shock Waves, 2021 - Springer
Changing the flow rate of reactants being injected into a rotating detonation combustor
(RDC) results in interesting behavior of the system. Prior studies have found that an increase …

Evaluation of the surrogates capacity to reproduce the laminar burning velocities and the sensitivity to stretching of a commercial kerosene under constant volume …

R Le Dortz, C Strozzi, J Sotton, M Bellenoue - Fuel, 2021 - Elsevier
These last years, aircraft manufacturers and environmental international bodies have set
drastic targets concerning turbo-engines pollution and consumption reduction. To reach the …

Deflagration/Autoignition/Detonation Transition Induced by Flame Propagation in an N-Decane/O2 /Ar Mixture

H Quintens, C Strozzi, R Zitoun… - Flow, Turbulence and …, 2019 - Springer
The aim of this study is to experimentally investigate the combustion regime transitions of a
single-component kerosene surrogate (n-decane). For this purpose, a deflagration is …

Experimental investigation on detonation dynamics through a reactivity sink

S Boulal, P Vidal, R Zitoun, T Matsumoto… - Combustion and Flame, 2018 - Elsevier
This article reports on an experimental investigation into dynamical behaviours of detonation
in non-uniform mixtures, generated from stoichiometric propane–oxygen, oxygen and …

Experimental investigation of ignition stability in a cyclic constant-volume combustion chamber featuring relevant conditions for air-breathing propulsion

Q Michalski, B Boust, M Bellenoue - Flow, Turbulence and Combustion, 2019 - Springer
Pressure-gain combustion concepts are developed around the world as solutions to reach
the ambitious target of the ultra-efficient aircraft road map for 2050 that requires a 20 …

Pressure-Angle Polars Obtaining Flow Field of Rotating Detonation

C Jiang, Y Wang, G Zhang - Combustion Science and Technology, 2024 - Taylor & Francis
Rotating detonation engines have been studied experimentally and numerically due to a
higher thermal efficiency in theory. Numerical simulations of the flow field inside the engine …

Analytical and numerical study of the expansion effect on the velocity deficit of rotating detonation waves

M Luan, S Zhang, Z Xia, S Yao… - Combustion Theory and …, 2020 - Taylor & Francis
In this work, a quasi-one-dimensional ZND model of detonation considering the expansion
process perpendicular to the detonation propagation direction is extended to the rotating …

[PDF][PDF] Nuclear Wave Rotor Bi-Modal Cycle for In-Space Propulsion

R Gosse, G Osborne, H Mahmood… - AIAA SCITECH 2024 …, 2024 - faculty.eng.ufl.edu
A ta fundamental level, in-space Electric Propulsion (EP) is limited by the power cycle's
ability to reject waste heat generated by its energy conversion process. This in turn produces …

A Review of Pressure Gain Combustion Solutions for Aerospace Propulsion

S Purushothaman, A Renuke… - … Expo: Power for …, 2022 - asmedigitalcollection.asme.org
Abstract Recent developments in Pressure Gain Combustion (PGC) technology have
demonstrated its ability to achieve higher thermal efficiencies and lower carbon emissions …

Fuel Injection Dynamics and Composition Effects on RDE Performance

M Gamba, V Raman - 2023 - osti.gov
Rotating detonation engines (RDEs) provide a promising route to substantially increasing
cycle efficiency in stationary gas turbines. Much of this increase relies on the ability to …