Streamline curvature computational programme for axial compressor performance prediction [PDF]
, 1987 Accurate prediction of overall performance is vital if the extremely high design and development costs of modern high speed compressors are to be minimised.
Barbosa, J. R.
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Three-Dimensional Flow and Performance Simulation of Multistage Axial Flow Compressors [PDF]
, 2000 \Yith the current develop111ent in computer technology and Computational Fluid D ...
Li, Y., Li, Yiguang
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Cascade Testing and CFD Applied to Gas Turbine Performance Improvement with Compressor Cleaning [PDF]
, 2010 With the growing interest in life cycle costs for heavy-duty gas turbines, equipment operators are investigating the trade off between performance improvements and associated maintenance costs. One of the key factors leading to performance degradation
Gannan, Aiad
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The application of multi-agent systems to the design of an intelligent geometry compressor [PDF]
, 2002 This thesis was submitted for the degree of Doctor of Philosophy and awarded by Brunel University.In this research, a multi-agent approach was applied to the design of a large axial flow compressor in order to optimise performance and to greatly enlarge ...
Morgan, Gwyn
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Aerodynamic design and numerical simulation of mixed-axial flow multi-stage compressor
Zhongguo Jianchuan Yanjiu, 2018 [Objectives] The performance of a gas turbine engine can be determined by the performance of the compressor. As one of the core components of a gas turbine engine,the design of the compressor is of critical importance in the design of the engine overall.[
ZHANG Xiaoyang +3 more
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Stochastic axial compressor variable geometry schedule optimisation [PDF]
, 2011 The design of axial compressors is dictated by the maximisation of flow efficiency at on design conditions whereas at part speed the requirement for operation stability prevails.
Singh, R. +7 more
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Applied Sciences, 2021 Non-uniform inlet flows frequently occur in aircrafts and result in chronological distortions of total temperature and total pressure at the engine inlet.
Muhammad Umer Sohail +7 more
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The effect of upstream duct boundary layer growth and compressor blade lean angle variation on an axial compressor performance [PDF]
, 2010 The compressor of a gas turbine engine is extremely vulnerable on upstream duct- induced flow non-uniformities whether the duct is an engine intake or an interconnecting duct.
Templalexis, I. +3 more
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Numerical investigation of recess casing treatments in axial flow fans [PDF]
, 2003 T he casing treatment technique for the axial fan has never been more significant since its potential applications were recognized in gas turbines, tunnel ventilation and many other industrial applications where the axial fan would benefit from the ...
Ghila, Abdurazag M.
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Energies, 2020 The tip clearance has an important effect on the performance of an engine compressor. While the impact of tip clearance on a concentric compressor has been widely explored in previous research, the flow field distribution of an eccentric compressor has ...
Chao Jiang +3 more
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