Volume 1: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Wind Turbine Technology 2011
DOI: 10.1115/gt2011-46437
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Virtual Gas Turbines: Geometry and Conceptual Description

Abstract: This paper documents the construction of a Virtual Engine, with particular reference to its geometry and conceptual description.. The phrase Virtual Engine denotes a system which allows simulations of whole gas-turbine engines to be undertaken at any desired level of fidelity or physical modeling. In order to be of any practical use, the system must allow the computations to be setup as automatically as possible and needs to contain provisions for the exchange of boundary data between adjacent computational do… Show more

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Cited by 22 publications
(12 citation statements)
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“…The proposed method has been implemented in the in-house CFD solver AU3X [18,19]. AU3X solves the unsteady Reynolds-Averaged Navier-Stokes (RANS) equations implicitly on unstructured meshes using a cell-centered finite volume scheme.…”
Section: Solution Methodsmentioning
confidence: 99%
“…The proposed method has been implemented in the in-house CFD solver AU3X [18,19]. AU3X solves the unsteady Reynolds-Averaged Navier-Stokes (RANS) equations implicitly on unstructured meshes using a cell-centered finite volume scheme.…”
Section: Solution Methodsmentioning
confidence: 99%
“…The test vehicle for this study is AU3X [9], [10], a cell-centred finite-volume code used for solving the unsteady Favre-averaged Navier Stokes equations on unstructured meshes in both time and frequency domains. The solver obtains steady solutions via pseudo-time marching and timeaccurate solutions by dual-time stepping.…”
Section: Unstructured Finite-volume Cfd Solver a Overviewmentioning
confidence: 99%
“…This article presents an approach that can significantly reduce the time-cost in preliminary thermal-mechanical design, which in nature is highly iterative and involves large number of boundary condition data. The methodology is built upon the feature-based system previously proposed by the authors (29) and allows sets of BCs to be represented parametrically. The parameterisation of BCs is associated to engine assembly features enabling the establishment of the one-to-one mapping between its geometric model and related thermal-mechanical model.…”
Section: March 2018mentioning
confidence: 99%
“…The authors previously presented a feature-based geometric modelling system for the representation of gas turbine assemblies (29) . This system is based on abstraction.…”
Section: Parametric Boundary Condition Representation 21 Bc Configurmentioning
confidence: 99%