Axial compressor blades tip leakage flow control using natural aspiration. [PDF]
Sci Rep, 2023 Nejad PG, Zenouz RT.
europepmc +1 more source
Parametric study of advanced multistage axial-flow compressors [PDF]
Axial flow compressor study to increase pressure ratio and reduce overall ...
Bryans, A. C., Miller, M. L.
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An integral equation solution for multistage turbomachinery design calculations [PDF]
A method was developed to calculate flows in multistage turbomachinery. The method is an extension of quasi-three-dimensional blade-to-blade solution methods.
Mcfarland, Eric R.
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Noise Reduction Studies for a Multistage Axial Flow Transonic Compressor [PDF]
The Journal of the Acoustical Society of America, 1967 It is the purpose of this paper to describe an aircraft-type transonic compressor built especially for noise research studies and to present some preliminary results. This compressor is unique in that it is adjustable over a very wide range of operating conditions.
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Techno-Economic Optimization of Multistage Membrane Processes with Innovative Hollow Fiber Modules for the Production of High-Purity CO2 and CH4 from Different Sources. [PDF]
Ind Eng Chem Res, 2022 Abejón R, Casado-Coterillo C, Garea A.
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Computational thermo-fluid dynamics contributions to advanced gas turbine engine design [PDF]
The design practices for the gas turbine are traced throughout history with particular emphasis on the calculational or analytical methods. Three principal components of the gas turbine engine will be considered: namely, the compressor, the combustor and
Adamczyk, J. J. +2 more
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Case wall pressures in a multistage axial compressor with tip clearance variation
Journal of Propulsion and Power, 1996 Large cyclical pressure excursions from stator-averaged values are observed on the suction side of a rotor blade at the case wall in a multistage compressor as the rotor moves relative to the stator. The pressure changes correlate well with stator relative position, occur in the passage away from the blade, and are only slightly modified by tip ...
Moyle, I.N., Shreeve, R.P., Walker, G.J.
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The discipline research in turbomachinery, which is directed toward building the tools needed to understand such a complex flow phenomenon, is based on the fact that flow in turbomachinery is fundamentally unsteady or time dependent.
Adamczyk, John J. +4 more
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Design of a Supercritical CO2 Compressor for Use in a 1 MWe Power Cycle. [PDF]
ACS Omega, 2021 Jiang P, Wang B, Tian Y, Xu X, Zhao L.
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Enhancing aeropropulsion research with high-speed interactive computing [PDF]
NASA-Lewis has committed to a long range goal of creating a numerical test cell for aeropropulsion research and development. Efforts are underway to develop a first generation Numerical Propulsion System Simulation (NPSS).
Arpasi, Dale J. +2 more
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