scholarly journals An Early Stage of Aerosol Particle Transport in Flows Past Periodic Arrays of Clear Staggered Obstructions: A Computational Study

2014 ◽  
Vol 48 (12) ◽  
pp. 1299-1307 ◽  
Author(s):  
Kuang C. Lin ◽  
Hairong Tao ◽  
Kuan-Wei Lee
2021 ◽  
Vol 33 (8) ◽  
pp. 089906
Author(s):  
Ali Khosronejad ◽  
Seokkoo Kang ◽  
Fabian Wermelinger ◽  
Petros Koumoutsakos ◽  
Fotis Sotiropoulos

Particuology ◽  
2016 ◽  
Vol 28 ◽  
pp. 102-113 ◽  
Author(s):  
Xiaole Chen ◽  
Wenqi Zhong ◽  
Josin Tom ◽  
Clement Kleinstreuer ◽  
Yu Feng ◽  
...  

2015 ◽  
Vol 17 (32) ◽  
pp. 20522-20529 ◽  
Author(s):  
Luigi Cigarini ◽  
Davide Vanossi ◽  
Federica Bondioli ◽  
Claudio Fontanesi

The dynamics of the early stage reaction between benzyl alcohol and Fe(acetylacetonate)3 is studied by exploiting the Dynamic Reaction Coordinate (DRC) approach, at the PBE0/6-31G* level of theory.


1992 ◽  
Vol 20 (6) ◽  
pp. 573-581 ◽  
Author(s):  
James K. Briant ◽  
Duane D. Frank ◽  
Anthony C. James ◽  
L. Loren Eyler

Author(s):  
Jerome Le Moine ◽  
P. K. Senecal ◽  
Sebastian A. Kaiser ◽  
Victor M. Salazar ◽  
Jon W. Anders ◽  
...  

This paper reports the validation of a three-dimensional numerical simulation of the mixture preparation in a direct-injection hydrogen-fueled engine. Computational results from the commercial code CONVERGE are compared to the experimental data obtained from an optically accessible engine. The geometry used in the simulation is a passenger-car sized, four-stroke, spark-ignited engine. The simulation includes the geometry of the combustion chamber as well as the intake and exhaust ports. The hydrogen is supplied at 100 bar from a centrally located injector with a single-hole nozzle. The comparison between the simulation and experimental data is made on the central vertical plane. The fuel mole concentration and flow field are compared during the compression stroke at different crank angles. The comparison shows good agreement between the numerical and experimental results during the early stage of the compression stroke. The penetration of the jet and the interaction with the cylinder walls are correctly predicted. The fuel spreading is under predicted which results in differences in flow field and fuel mixture during the injection between experimental and numerical results. At the end of the injection, the fuel distribution shows some disagreement which gradually increases during the rest of the simulation.


2019 ◽  
Author(s):  
S. C. Saha ◽  
M. S. Islam ◽  
M. Rahimi-Gorji ◽  
M. M. Molla

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