Review of combustion stabilization for hypersonic airbreathing propulsion
A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …
Large eddy simulation of turbulent supersonic hydrogen flames with OpenFOAM
A high-fidelity numerical solver, RYrhoCentralFoam, is developed based on OpenFOAM® to
simulate turbulent compressible reactive flows. It is designed for accurately simulating …
simulate turbulent compressible reactive flows. It is designed for accurately simulating …
Hydrogen combustion in gas turbines
The development of gas turbines using 100% hydrogen as fuel is an important step towards
the development of new energy and propulsion technologies using zero carbon fuels. This …
the development of new energy and propulsion technologies using zero carbon fuels. This …
A combined oscillation cycle involving self-excited thermo-acoustic and hydrodynamic instability mechanisms
D Fredrich, WP Jones, AJ Marquis - Physics of Fluids, 2021 - pubs.aip.org
The paper examines the combined effects of several interacting thermo-acoustic and
hydrodynamic instability mechanisms that are known to influence self-excited combustion …
hydrodynamic instability mechanisms that are known to influence self-excited combustion …
Numerical investigate on flow process and mixing characteristics of hydrogen/aluminum powder two-phase fuel under different inlet and injection conditions
H Ding, C Zhuo, H Deng, X Chen, B Sun - International Journal of …, 2024 - Elsevier
The flow and mixing process of a hydrogen/aluminum powder two-phase fuel transverse jet
in a supersonic cross flow are simulated in this work using the Euler-Lagrangian scheme …
in a supersonic cross flow are simulated in this work using the Euler-Lagrangian scheme …
Numerical investigation on flame stabilization in DLR hydrogen supersonic combustor with strut injection
Flame stabilization in the DLR hydrogen supersonic combustor with strut injection was
numerically investigated by using an in-house large eddy simulation code developed on the …
numerically investigated by using an in-house large eddy simulation code developed on the …
Application of the sparse-Lagrangian multiple mapping conditioning approach to a model supersonic combustor
The Multiple Mapping Conditioning/Large Eddy Simulation (MMC-LES) model is extended
for the first time to high-speed, compressible flow conditions and validated against non …
for the first time to high-speed, compressible flow conditions and validated against non …
Experimental and numerical investigation of the transition progress of strut-induced wakes in the supersonic flows
C Liu, J Zhang, D Jia, P Li - Aerospace Science and Technology, 2022 - Elsevier
Strut serves as an effective and robust flameholder in a scramjet combustor, and the
resultant wakes have a great impact on the fuel mixing and flame stabilization. Present work …
resultant wakes have a great impact on the fuel mixing and flame stabilization. Present work …
Investigation of influence of detailed chemical kinetics mechanisms for hydrogen on supersonic combustion using large eddy simulation
Five detailed hydrogen combustion chemical kinetics mechanisms coupled with a partially
stirred reactor (PaSR) combustion model were applied with large eddy simulation (LES) to …
stirred reactor (PaSR) combustion model were applied with large eddy simulation (LES) to …
Large eddy simulation of reacting flow in a hydrogen jet into supersonic cross-flow combustor with an inlet compression ramp
M Zhao, T Zhou, T Ye, M Zhu, H Zhang - International Journal of Hydrogen …, 2017 - Elsevier
Large eddy simulation (LES) has been performed to investigate transverse hydrogen jet
mixing and combustion process in a scramjet combustor model with a compression ramp at …
mixing and combustion process in a scramjet combustor model with a compression ramp at …