Mixing and combustion modeling of hydrogen peroxide/kerosene shear-coaxial jet flame in lab-scale rocket engine
S Li, Y Ge, X Wei, T Li - Aerospace Science and Technology, 2016 - Elsevier
H 2 O 2/kerosene bipropellants are effective alternatives for toxic propellants currently in
use. The complex H 2 O 2/kerosene turbulent flow and combustion chemical reaction are …
use. The complex H 2 O 2/kerosene turbulent flow and combustion chemical reaction are …
Real-Gas-Flamelet-Model-Based Numerical Simulation and Combustion Instability Analysis of a GH2/LOX Rocket Combustor with Multiple Injectors
A large eddy simulation (LES) and combustion instability analysis are performed using
OpenFOAM for the multiple shear-coaxial injector combustor DLR-BKD (in German …
OpenFOAM for the multiple shear-coaxial injector combustor DLR-BKD (in German …
Coupled heat transfer analysis of thrust chambers with recessed shear coaxial injectors
J Song, B Sun - Acta Astronautica, 2017 - Elsevier
To investigate the effects of recessed lengths on combustion performance and heat loads in
LOX/methane thrust chambers with shear coaxial injectors, a coupled numerical …
LOX/methane thrust chambers with shear coaxial injectors, a coupled numerical …
CFD simulations of turbulent nonreacting and reacting flows for rocket engine applications
MJ Seidl, M Aigner, R Keller, P Gerlinger - The Journal of Supercritical …, 2017 - Elsevier
A consistent real gas framework based on a preconditioning scheme is implemented into the
CFD code TASCOM3D to simulate nonreacting and reacting turbulent flows with transcritical …
CFD code TASCOM3D to simulate nonreacting and reacting turbulent flows with transcritical …
Alternatives to the beta distribution in assumed PDF methods for turbulent reactive flow
PP Popov - Flow, Turbulence and Combustion, 2022 - Springer
This work addresses a shortcoming of the beta distribution when applied to assumed
probability density function (PDF) methods for reactive flow, such as the flamelet-progress …
probability density function (PDF) methods for reactive flow, such as the flamelet-progress …
Numerical Simulation of a GH2/LOx Single Injector Combustor and the Effect of the Turbulent Schmidt Number
A large-eddy simulation (LES) of a gaseous hydrogen/liquid oxygen (GH2/LOX) single-
injector rocket combustor is performed in this study. The Redlich–Kwong–Peng–Robinson …
injector rocket combustor is performed in this study. The Redlich–Kwong–Peng–Robinson …
[PDF][PDF] Numerische Simulation von Raketenbrennkammern mit transkritischer Einspritzung
M Seidl - 2018 - elib.dlr.de
Der spezifische Impuls Isp ist ein Maß für die Effizienz von Raketentriebwerken und das
Verhältnis von gewonnenem Impuls zur eingesetzten Treibstoffmenge. Für eine an den …
Verhältnis von gewonnenem Impuls zur eingesetzten Treibstoffmenge. Für eine an den …
Estudo numérico de chamas turbulentas não pré-misturadas através de modelos baseados no conceito de flamelets
DL Deon - 2016 - lume.ufrgs.br
A simulação numérica de chamas turbulentas é ainda hoje um desafio para as práticas de
mecânica dos fluidos computacional. Compreendendo que as abordagens numéricas mais …
mecânica dos fluidos computacional. Compreendendo que as abordagens numéricas mais …
Numerical Simulation of High-Pressure Combustion using Conditional Source-term Estimation
S De Graaf, SR Taylor, GR Hendra, N Christopher… - 2017 - elib.dlr.de
The applicability of Conditional Source-term Estimation (CSE) for high-pressure combustion
applications is investigated within the context of Reynolds Averaged Navier-Stokes …
applications is investigated within the context of Reynolds Averaged Navier-Stokes …
[CITATION][C] Wall Heat Flux Map** in Liquid Rocket Combustion Chamber with Different Jet Im**ement Angles
OS Pradeep, S Vigneshwaran, KP Kumar, K Jeyendran… - International Journal of …, 2017