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http://dx.doi.org/10.6108/KSPE.2018.22.6.072

Numerical Study of High Resolution Schemes for GH2/GO2 Rocket Combustor using Single Shear Coaxial Injector  

Jeong, Seung-Min (Department of Aerospace Engineering, Pusan National University)
Um, Jae-Ryeong (Satellite System Team, Korea Aerospace Industries LTD)
Choi, Jeong-Yeol (Department of Aerospace Engineering, Pusan National University)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.22, no.6, 2018 , pp. 72-83 More about this Journal
Abstract
In this study, a series of CFD analyses were carried out for a hydrogen rocket combustor with a single shear coaxial injector. A hybrid RANS/LES approach was used for the turbulent combustion analysis with a two-dimensional axisymmetric configuration. Three reaction mechanisms, three spatial discretization methods, and three levels of grid resolution were compared to determine an appropriate CFD approach. The performance of the CFD prediction were investigated by comparing the wall heat flux with experimental data. Investigation of the flow field results provides an insight into the characteristics of the turbulent reacting flow of a rocket combustor with a shear coaxial injector.
Keywords
Single Shear Coaxial Injector; Turbulent Combustion; Chemical Reaction Mechanism; High-Order Spatial Discretization Method; Grid Resolution;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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