Results 61 to 70 of about 4,842 (209)

Numerical simulation of the non-uniform flow in a full-annulus multi-stage axial compressor with the harmonic balance method

open access: yesAdvances in Mechanical Engineering, 2020
To improve the understanding of unsteady flow in modern advanced axial compressor, unsteady simulations on full-annulus multi-stage axial compressor are carried out with the harmonic balance method.
Haiou Sun   +4 more
doaj   +1 more source

The WINCOF-I code: Detailed description [PDF]

open access: yes
The performance of an axial-flow fan-compressor unit is basically unsteady when there is ingestion of water along with the gas phase. The gas phase is a mixture of air and water vapor in the case of a bypass fan engine that provides thrust power to an ...
Mullican, A., Murthy, S. N. B.
core   +1 more source

Detection of Rotor Forced Response Vibrations Using Stationary Pressure Transducers in a Multistage Axial Compressor

open access: yesInternational Journal of Rotating Machinery, 2015
Blade row interactions in turbomachinery can lead to blade vibrations and even high cycle fatigue. Forced response conditions occur when a forcing function (such as impingement of stator wakes) occurs at a frequency that matches the natural frequency of ...
William L. Murray, Nicole L. Key
doaj   +1 more source

End-wall boundary layer measurements in a two-stage fan [PDF]

open access: yes
Detailed flow measurements made in the casing boundary layer of a two-stage transonic fan are summarized. These measurements were taken at a station upstream of the fan, between all blade rows, and downstream of the last row.
Ball, C. L., Reid, L., Schmidt, J. F.
core   +1 more source

Design optimization of a multi-stage axial compressor using through flow and a database of optimal airflows

open access: yesJournal of the Global Power and Propulsion Society, 2018
The basic tool set to design multi-stage axial compressors consists of fast codes for throughflow and blade-to-blade analysis. Detailed blade row design is conducted with 3D CFD, mainly to control the end wall flow.
Markus Schnoes   +2 more
doaj   +1 more source

Stalled and stall-free performance of axial-flow compressor stage with three inlet-guide-vane and stator-blade settings [PDF]

open access: yes
The performance of the first stage of a transonic, multistage compressor was mapped over a range of inlet-guide-vane and stator-blade settings. Both stall-free and deep-stall performance data were obtained.
Cunnan, W. S.   +2 more
core   +1 more source

A theory of post-stall transients in multistage axial compression systems [PDF]

open access: yes
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.
core   +1 more source

Blade selection for a modern axial-flow compressor [PDF]

open access: yes
The procedures leading to successful design of an axial flow compressor are discussed. The three related approaches to cascade selection are: (1) experimental approach which relies on the use of experimental results from identical cascades to satisfy the
Wright, L. C.
core   +1 more source

Considerations for High-Fidelity Modeling of Unsteady Flows in a Multistage Axial Compressor

open access: yesInternational Journal of Turbomachinery, Propulsion and Power
This paper presents the development and validation of a high-fidelity, unsteady, computational fluid dynamics (CFD) model of the Purdue 3-Stage Axial Research Compressor. A grid convergence study assesses the spatial discretization accuracy of the single-
Douglas R. Matthews, Nicole L. Key
doaj   +1 more source

Numerical Simulation of Surge in Axial Compressor

open access: yesInternational 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
doaj   +1 more source

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