Entropy generation and CO2 emission in presence of pulsating oscillations in a bifurcating thermoacoustic combustor with a Helmholtz resonator at off-design …
In this work, we develop a 2D numerical model of a Y-shaped bifurcating combustor with a
Helmholtz resonator attached. Propane (C 3 H 8) is fueled and burnt with air by applying …
Helmholtz resonator attached. Propane (C 3 H 8) is fueled and burnt with air by applying …
Numerical investigation of supercritical combustion dynamics in a multi-element LOx–methane combustor using flamelet-generated manifold approach
A Sharma, A De, SS Kumar - Physics of Fluids, 2023 - pubs.aip.org
The article investigates liquid oxygen (LOx)–methane supercritical combustion dynamics in
a multi-element rocket-scale combustor using large eddy simulation (LES). A complex …
a multi-element rocket-scale combustor using large eddy simulation (LES). A complex …
Effect of jet splitting using passive strut on the performance and thermoacoustic characteristics of a scramjet combustor
A scramjet engine offers a potential route to achieve supersonic speeds using airbreathing
engines. Achieving proper mixing and combustion poses a challenge due to the supersonic …
engines. Achieving proper mixing and combustion poses a challenge due to the supersonic …
Brief Review of Recent Achievements in the Flamelet Manifold Selection and Probability Density Distribution for Flamelet Manifold Variables
G Yu, B Li - Journal of Energy Resources …, 2024 - asmedigitalcollection.asme.org
The flamelet model is a commonly used tool for turbulent combustion simulations in the
engineering field due to its computational efficiency and compatibility with complex chemical …
engineering field due to its computational efficiency and compatibility with complex chemical …
Wall heat transfer prediction in CH4/O2 and H2/O2 rocket thrust chambers using a non-adiabatic flamelet model
N Perakis, OJ Haidn - Acta Astronautica, 2020 - Elsevier
The current work presents the extension of the flamelet model for turbulent combustion
calculations to account for deviations from adiabatic conditions. The aforementioned …
calculations to account for deviations from adiabatic conditions. The aforementioned …
Investigation of injector-coupled combustion dynamics in a methane–oxygen combustor using large eddy simulation and dynamic mode decomposition
A Sharma, A De, S Kumar - Physics of Fluids, 2024 - pubs.aip.org
This paper uses a reactive flow large eddy simulation (LES) and decomposition techniques
to study combustion instabilities in a methane–oxygen combustor. This work examines two …
to study combustion instabilities in a methane–oxygen combustor. This work examines two …
Modelling of pulsating inverted conical flames: a numerical instability analysis
L da Costa Ramos, LF Figueira da Silva… - … Theory and Modelling, 2022 - Taylor & Francis
The study of combustion-thermoacoustic instabilities is a topic of interest in the development
of engines. However, the modelling of these systems involves a high computational burden …
of engines. However, the modelling of these systems involves a high computational burden …
Transported PDF modeling of compressible turbulent reactive flows by using the Eulerian Monte Carlo fields method
Although the transported probability density function (PDF) method has been developed for
decades, its application has been mainly focused on the low-Mach number flow problems …
decades, its application has been mainly focused on the low-Mach number flow problems …
Flamelet modeling of transverse thermo-acoustic instability in a multi-element combustor
Combustion instability resulting from thermo-acoustic interaction is a serious issue in
highpower, high-energy density propulsion devices like rocket engines, gas turbines and …
highpower, high-energy density propulsion devices like rocket engines, gas turbines and …
Analysis of self-excited combustion instability in a sub-scale rocket engine using large Eddy simulation
This paper invokes a reactive flow large eddy simulation (LES) framework to simulate
combustion instabilities in a sub-scale rocket combustion chamber. A model rocket …
combustion instabilities in a sub-scale rocket combustion chamber. A model rocket …