Modeling of viscous flows in two-dimensional turbomachinery cascade via viscous-inviscid interaction method

Yusoff, M. Z. and Hussein, I. and Yusaf, T. and Ahmad, Z. (2005) Modeling of viscous flows in two-dimensional turbomachinery cascade via viscous-inviscid interaction method. Institution of Engineers, Malaysia. Journal , 66 (3). pp. 14-20. ISSN 0126-513X

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A two-dimensional time-accurate time-marching viscous flow solver employing the viscous-inviscid interaction method
suitable for turbomachinery applications is described. The inviscid main flow solver uses the second-order accurate cellvertex finite-volume spatial discretisation and fourth-order accurate Runge-Kutta temporal integration. The viscous effect due to boundary layer development on the blade surfaces and wakes are modelled using an independent one-dimensional boundary layer subroutine capable of modelling laminar, transition and fully turbulent flows. The solver has been applied to subsonic, transonic and supersonic flow in a cascade of nozzle blades. The results are compared with the experimental data and they showed very good agreement

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Item Type: Article (Commonwealth Reporting Category C)
Refereed: Yes
Item Status: Live Archive
Depositing User: Ms Leslie Blay
Faculty / Department / School: Historic - Faculty of Engineering and Surveying - No Department
Date Deposited: 24 May 2010 02:51
Last Modified: 28 Nov 2013 01:27
Uncontrolled Keywords: boundary layer; CFD; time-marchin; turbine; turbomachinery; viscous
Fields of Research (FoR): 09 Engineering > 0915 Interdisciplinary Engineering > 091508 Turbulent Flows
09 Engineering > 0913 Mechanical Engineering > 091399 Mechanical Engineering not elsewhere classified
09 Engineering > 0915 Interdisciplinary Engineering > 091504 Fluidisation and Fluid Mechanics
Socio-Economic Objective (SEO): E Expanding Knowledge > 97 Expanding Knowledge > 970109 Expanding Knowledge in Engineering

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