Surface tension and evaporation behavior of liquid fuel droplets at transcritical conditions: Towards bridging the gap between molecular dynamics and continuum simulations-Reference-Cited by-同舟云学术

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Surface tension and evaporation behavior of liquid fuel droplets at transcritical conditions: Towards bridging the gap between molecular dynamics and continuum simulations

Published:2024-02 Issue: Volume:358 Page:130187
ISSN:0016-2361
Container-title:Fuel
language:en
Short-container-title:Fuel

Author:

Jangale Prajesh,Hosseini Ehsan,Zakertabrizi Mohammad,Jarrahbashi Dorrin

Funder

Texas A and M University

High Performance Research Computing, Texas A and M University

National Science Foundation

Publisher

Elsevier BV

Subject

Organic Chemistry,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering

Reference93 articles.

1. Hersch M, Rice EJ. Gaseous-hydrogen liquid-oxygen rocket combustion at supercritical chamber pressures; 1967.

2. Oefelein JC. Thermophysical characteristics of shear-coaxial LOX–H2 flames at supercritical pressure. Proc Combust Inst 2005;30(2):2929–37.

3. Harrje DT. Liquid propellant rocket combustion instability; 1972.

4. Direct numerical simulations of O/H temporal mixing layers under supercritical conditions;Okong';AIAA J,2002

5. Direct numerical simulations of supercritical fluid mixing layers applied to heptane–nitrogen;Miller;J Fluid Mech,2001

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Computational Analysis of Secondary Droplet Breakup at Transcritical Conditions with Surface Tension Effects;AIAA SCITECH 2024 Forum;2024-01-04

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