Numerical Simulation of Surge in Axial Compressor
International Journal of Rotating Machinery, 2012 The object of this paper is to provide a reliable tool to simulate the stationary and transient operation performances in multistage axial compression systems, especially poststall behavior.
Wenhai Du, Olivier Léonard
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A theory of post-stall transients in multistage axial compression systems [PDF]
A theory is presented for post stall transients in multistage axial compressors. The theory leads to a set of coupled first-order ordinary differential equations capable of describing the growth and possible decay of a rotating-stall cell during a ...
Greitzer, E. M., Moore, F. K.
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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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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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Development and Applications of a Stage Stacking Procedure [PDF]
, 2012 The preliminary design of multistage axial compressors in gas turbine engines is typically accomplished with mean-line methods. These methods, which rely on empirical correlations, estimate compressor performance well near the design point, but may ...
Adamczyk, John J. +2 more
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Static and dynamic analysis of the closing rotor balancing device of the multistage centrifugal pump [PDF]
, 2014 The closing rotor balancing device of the multistage centrifugal pump with regulator of pressure difference acts as the end seal and the hydrostatic bearing with self-regulating gap and fluid leakages.
Pavlenko, Ivan Volodymyrovych +2 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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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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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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Discussion: “Four Pad Tilting Pad Bearing Design and Application for Multistage Axial Compressors” (Nicholas, J. C., and Kirk, R. G., 1982, ASME J. Lubr. Technol., 104, pp. 523–529) [PDF]
, 1982 Ronald D. Flack
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