Incompressible versus compressible large eddy simulation for the identification of premixed flame dynamics
The present work compares the respective advantages and disadvantages of compressible
and incompressible computational fluid dynamics (CFD) formulations when used for the …
and incompressible computational fluid dynamics (CFD) formulations when used for the …
Unsteady multi-component simulations dedicated to the impact of the combustion chamber on the turbine of aeronautical gas turbines
C Koupper - 2015 - theses.hal.science
Nowadays, engines powering modern and large commercial or military aircraft essentially
rely on gas turbine technologies. Since the first prototypes built in the 40's, the efficiency and …
rely on gas turbine technologies. Since the first prototypes built in the 40's, the efficiency and …
Direct Numerical Simulation of combustion near a carbonaceous surface in a quiescent flow
In this work, unsteady gasification and oxidation of carbonaceous materials with gas-phase
combustion under oxy-combustion conditions is studied. An original analytical solution is …
combustion under oxy-combustion conditions is studied. An original analytical solution is …
CFD analysis on swirl angle effect in gas turbine combustion chamber
RG Bhuvana, SA Srinivasan… - IOP Conference Series …, 2018 - iopscience.iop.org
Swirl vanes are used for imparting swirling motion to the flow. These swirl vanes with its
vanes induce the air circulation in order to create a turbulence at the primary zone of the …
vanes induce the air circulation in order to create a turbulence at the primary zone of the …
Evaluation and Validation of Two-Phase Flow Numerical Simulations Applied to an Aeronautical Injector Using a Lagrangian Approach
J Tillou, J Leparoux, J Dombard… - … Expo: Power for …, 2020 - asmedigitalcollection.asme.org
Non-reactive Lagrangian two-phase flow Large-Eddy Simulations (LES) of an industrial
aeronautical injector are carried out with the compressible AVBP code and compared with …
aeronautical injector are carried out with the compressible AVBP code and compared with …
[PDF][PDF] PERFORMANCE AND EMISSION OF SWIRL BURNER WITH DIFFERENT SWIRL NUMBERS USING PALM, COCONUT AND JATROPHA OIL BIODIESEL
NBA RAHIM - 2017 - eprints.utm.my
Biodiesel is used as an alternative invaluable fuel in reducing the effect of global warming,
greenhouse-gas emissions, and severe climate changes. It is also considered as promising …
greenhouse-gas emissions, and severe climate changes. It is also considered as promising …
Effect of Aromatics in Jet Fuels on Spray Characteristics Downstream of an Aeronautical Pressure Swirl Atomizer
J Leparoux, R Lecourt… - … Expo: Power for …, 2016 - asmedigitalcollection.asme.org
Standard aeronautic fuels have a lower limit of aromatics of 8%(by volume) with about 18%
for regular Jet A1. It has been shown that aromatics contained in Jet fuel have an impact on …
for regular Jet A1. It has been shown that aromatics contained in Jet fuel have an impact on …
[PDF][PDF] Sensitivity analysis to the normal grid-resolution in a turbulent channel flow using large-eddy simulations
J Dombard, G Iaccarino - Center for Turbulence Research, 2012 - stanford.edu
Pressure losses are of primary importance in the design of gas turbines (Lefebvre 1999).
They drive the mass-flow rate between the liner and the combustion chamber through …
They drive the mass-flow rate between the liner and the combustion chamber through …
모델가스터빈연소기내선회기Vane 의두께가Counter-rotating 선회유동에미치는영향
이상호, 진유인, 유경원, 이지근 - 한국추진공학회학술대회논문집, 2016 - dbpia.co.kr
선회기 Vane 의 두께가 모델 가스터빈 연소기 내에 형성되는 선회유동 특성에 미치는 영향이
실험적으로 조사되었다. 모델 연소기는 가스터빈 연소기를 직사각형으로 모사하여 …
실험적으로 조사되었다. 모델 연소기는 가스터빈 연소기를 직사각형으로 모사하여 …
Effect of Reynolds Numbers on Counter-rotating Swirling Flow in a Model Gas Turbine Combustor
S Lee, Y Jin, G Ryu, J Lee - 대한기계학회춘추학술대회, 2015 - dbpia.co.kr
The characteristics of swirling flow in a model gas turbine combustor, which is one of the
most important phenomenon for efficiency and flame stabilization in gas turbines, were …
most important phenomenon for efficiency and flame stabilization in gas turbines, were …