Combustion characteristics and misfire mechanism of a passive pre-chamber direct-injection gasoline engine

H Zhou, S Meng, Z Han - Fuel, 2023 - Elsevier
Engine combustion characteristics and misfire phenomena in a turbocharged direct-injection
gasoline engine with a pre-chamber are studied through multi-dimensional modeling of the …

On the gradient diffusion hypothesis and passive scalar transport in turbulent flows

DP Combest, PA Ramachandran… - Industrial & …, 2011 - ACS Publications
A discussion of modeling passive scalar transport in turbulent flows is given. Several
methods employed to close the scalar-flux term⟨ u′ ϕ′⟩ that arises during Reynolds …

Uncertainty quantification analysis of Reynolds-averaged Navier–Stokes simulation of spray swirling jets undergoing vortex breakdown

J Liberatori, RM Galassi, M Valorani… - … Journal of Spray and …, 2023 - journals.sagepub.com
The computational fluid dynamics-based design of next-generation aeronautical combustion
chambers is challenging due to many geometrical and operational parameters to be …

Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors

A Andreini, T Bacci, M Insinna, L Mazzei… - Aerospace Science and …, 2018 - Elsevier
The accurate prediction of the fluid dynamic conditions at the exit of gas turbine combustors
are of paramount importance in the aero-thermal design of the aero-engine. In fact, both the …

Combustion Characterization in a Diffusive Gas Turbine Burner for Hydrogen-Compliant Applications

S Carusotto, P Goel, M Baratta, DA Misul, S Salvadori… - Energies, 2022 - mdpi.com
The target of net-zero emissions set by the 2015 Paris Agreement has strongly
commissioned the energy production sector to promote decarbonization, renewable sources …

[图书][B] A 3d coupled approach for the thermal design of aero-engine combustor liners

L Mazzei, A Andreini, B Facchini, L Bellocci - 2016 - asmedigitalcollection.asme.org
The adoption of lean burn combustion to limit NOx emissions of modern aero-engines
imposes a drastic reduction of air dedicated to cooling combustor dome and liners. In the …

Reynolds analogy in combustor modeling

LY Jiang, I Campbell - International Journal of Heat and Mass Transfer, 2008 - Elsevier
The Reynolds analogy concept has been used in almost all turbulent reacting flow RANS
(Reynolds-averaged Navier–Stokes) simulations, where the turbulence scalar transfers in …

[HTML][HTML] Large eddy simulation of a supersonic lifted hydrogen flame: Impacts of Lewis, turbulent Schmidt and Prandtl numbers

R Zhu, Z Huang, C Xu, X Fang, H Zhang, M Davy - Physics of Fluids, 2024 - pubs.aip.org
Parametric large eddy simulations (LES) of a supersonic lifted hydrogen flame are reported.
The emphases are on two aspects: impacts of (1) Lewis number (Le i of the ith species) and …

Assessment of aero-thermal design methodology for effusion cooled lean burn annular combustors

A Andreini, B Facchini, L Mazzei… - … Expo: Power for …, 2014 - asmedigitalcollection.asme.org
Increasingly stringent limitations imposed on aircraft engine emissions have led many
manufacturers toward lean combustion technology, which involves a relevant increase in …

Investigation of passive scalar mixing in a turbulent free jet using simultaneous LDV and cold wire measurements

A Darisse, J Lemay, A Benaïssa - International journal of heat and fluid flow, 2013 - Elsevier
A slightly heated turbulent round jet at high Reynolds number (Re D= 1.5× 10 5) was studied
using simultaneous Laser Doppler Velocimetry and cold wire thermometry measurements …