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http://dx.doi.org/10.6108/KSPE.2013.17.6.048

Study on Thermophysical Property Characteristics of a 4 Species Kerosene Surrogate in a Swirl Injector at Supercritical Pressure Condition  

Kim, Kukjin (Department of Aerospace and Mechanical Engineering, Korea Aerospace University)
Heo, Junyoung (Department of Aerospace and Mechanical Engineering, Korea Aerospace University)
Sung, Honggye (School of Aerospace and Mechanical Engineering, Korea Aerospace University)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.17, no.6, 2013 , pp. 48-58 More about this Journal
Abstract
Characteristics of thermophysical properties and flow structures in a swirl injector at supercritical pressure have been investigated using the kerosene surrogate consisting of four species and various ideal and real gas equations of state. The quantitative comparisons of thermophysical properties for equations of state have been performed. Also, a large eddy simulation and preconditioning technique for getting an effective convergence rate are applied to analyze turbulent flow in a swirl injector. The flow characteristics in the injector has significantly different behaviors depending on the equations of state due to the different thermophysical properties in the injector. The Redlich-Kwong-Peng-Robinson equation of state provides the most suitable results in the wide range of temperature.
Keywords
Supercritical Condition; Swirl Injector; Kerosene; Surrogate Model; Real Gas Equation of State;
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Times Cited By KSCI : 1  (Citation Analysis)
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