Results 11 to 20 of about 84,868 (188)
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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Preliminary aerothermal design of axial compressors [PDF]
, 2013 This dissertation documents a compressor preliminary design study conducted by the author in fulfilment of his MSc thesis requirements. The compressor is intended for a new development engine within the 20Klbf thrust category, planned to be used on a ...
Piscopo, Giovanni
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An experimental and computational analysis of compressor cascades with varying surface roughness [PDF]
, 2009 This thesis presents a CFD and experimental analysis associated with the parameter compressor fouling and a CFD analysis associated with the parameter on-line compressor washing of industrial gas turbines.
Fouflias, Dimitrios
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The New Chapter of Transonic Compressor Cascade Design at the DLR [PDF]
, 2023 The design of compressor blades has been transformed by the advent of optimization algorithms, allowing designers to focus on finding the best optimization strategy for a desired application.
Hergt, Alexander Silvio +3 more
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Experiment and Numerical Simulation of Aerodynamic Performance of Compressor with Damaged Blades [PDF]
Journal of Applied Fluid MechanicsThe present work attempted to lay a basis for evaluating the compressor aerodynamic performance in service environments. To achieve this goal, a low-speed compressor along with a transonic compressor rotor (NASA Rotor37) were studied.
H. Sun, Z. Wang, G. Luo
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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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The Current Gap between Design Optimization and Experiments for Transonic Compressor Blades
International Journal of Turbomachinery, Propulsion and Power, 2023 The successful design of compressor blades through numerical optimization relies on accurate CFD-RANS solvers that are able to capture the general performance of a given design candidate.
Edwin Joseph Munoz Lopez +4 more
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Advanced Compressor Loss Correlations, Part I: Theoretical Aspects
International Journal of Rotating Machinery, 1997 Reliable efficiency calculation of high-subsonic and transonic compressor stages requires a detailed and accurate prediction of the flow field within these stages.
M. T. Schobeiri
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Engineering Applications of Computational Fluid Mechanics, 2021 Design optimization of transonic airfoils for rotary blades is a challenging subject that remarkably affects the stage and overall performance of axial-flow compressors.
A. Zeinalzadeh, M.R. Pakatchian
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Advances in Mechanical Engineering, 2017 Numerical simulation has been conducted on a transonic contra-rotating axial compressor to investigate the shock wave and flow characteristics under various operation conditions.
Hanru Liu +3 more
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