Large eddy simulations of high pressure rocket propellant #3 aviation kerosene spay in pressurized quiescent environments-Reference-Cited by-同舟云学术

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Large eddy simulations of high pressure rocket propellant #3 aviation kerosene spay in pressurized quiescent environments

Published:2021-08-12 Issue: Volume: Page:1-16
ISSN:1556-7036
Container-title:Energy Sources, Part A: Recovery, Utilization, and Environmental Effects
language:en
Short-container-title:Energy Sources, Part A: Recovery, Utilization, and Environmental Effects

Author:

Liu Tao¹²³,Xiong Yanyi⁴,Zhao Dongmei¹^ORCID

Affiliation:

1. School of Computer Science and Technology, Southwest University of Science and Technology, Mianyang, China

2. Sichuan Civil-Military Integration Institute, Mianyang, China

3. Key Laboratory of Hypersonic Ramjet Technology, China Aerodynamics Research and Development Center, Mianyang, China

4. China Shipbuilding Industry Corp 713th Research Institute, Zhengzhou, China

Funder

Open Fund of Key Laboratory of hypersonic ramjet Technology

Doctoral Fund of Southwest University of Science and Technology

Publisher

Informa UK Limited

Subject

Energy Engineering and Power Technology,Fuel Technology,Nuclear Energy and Engineering,Renewable Energy, Sustainability and the Environment

Link

https://www.tandfonline.com/doi/pdf/10.1080/15567036.2021.1965265

Reference26 articles.

1. Numerical Simulation of Pressure-Swirl Spray Dispersion by Using Eulerian-Lagrangian Method

2. JP-8 and JP-5 as Compression Ignition Engine Fuel

3. Large Eddy Simulation of High Reynolds Number Nonreacting and Reacting JP-8 Sprays in a Constant Pressure Flow Vessel With a Detailed Chemistry Approach

4. LES of a swirl-stabilized kerosene spray flame with a multi-component vaporization model and detailed chemistry

5. On the two‐way interaction between homogeneous turbulence and dispersed solid particles. I: Turbulence modification

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