Results 21 to 30 of about 18,174 (265)

An Analytical Study on the Effect of Non-Uniform Vane Spacing on Forced Response Reduction in a Mistuned Blisk Rotor in a Multistage Axial Compressor

open access: hybridVolume 10A: Structures and Dynamics — Aerodynamics Excitation and Damping; Bearing and Seal Dynamics; Emerging Methods in Engineering Design, Analysis, and Additive Manufacturing
Stators with non-uniform vane spacing (NUVS) have been sought as an effective way to reduce the rotor forced response at certain resonance crossing of concern.
Yujun Leng   +2 more
openalex   +2 more sources

Unsteady Kinematics of Multistage Axial Compressor Shrouded Cavity Flows

open access: bronze, 2020
An experimental investigation has been performed in a low-speed shrouded multistage axial compressor to investigate the impact of mainstream flow on unsteady shrouded cavity flow.
Jaehyoung Lee   +6 more
openalex   +2 more sources

Large eddy simulation of flows in industrial compressors: a path from 2015 to 2035. [PDF]

open access: yesPhilos Trans A Math Phys Eng Sci, 2014
A better understanding of turbulent unsteady flows is a necessary step towards a breakthrough in the design of modern compressors. Due to high Reynolds numbers and very complex geometry, the flow that develops in such industrial machines is extremely ...
Gourdain N   +3 more
europepmc   +3 more sources

A one-dimensional stage un-stacking approach to reveal flow angles and speeds in a multistage axial compressor at the design operating point

open access: goldMechanics & Industry, 2019
Stage stacking methods commonly use a one-dimensional (1D) through flow analysis at the mean line to design individual axial compressor stages and stack these to form a multistage axial compressor.
Fu Hai Alan Koh, E. Y. K. Ng
openalex   +2 more sources

End-to-end design of multistage high-pressure axial compressor for a promising aviation gas turbine engine [PDF]

open access: goldJournal of Physics: Conference Series
The paper describes the results of an end-to-end design of a multistage high-pressure axial compressor for a promising aircraft engine. The design included the steps of initial design and detailed fine-tuning of the working process using three ...
Evgeny S. Goryachkin, I. Kudryashov
openalex   +2 more sources

Surging Limits of Multistage Axial-Flow Compressors.

open access: bronzeTRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B, 1992
Yoshimi Nishihara
openaire   +4 more sources

Poster: Boundary Layer Separations in a Multistage Axial Compressor [PDF]

open access: hybrid67th Annual Meeting of the APS Division of Fluid Dynamics - Gallery of Fluid Motion, 2014
Natalie R. Smith, Nicole L. Key
openaire   +3 more sources

Impact Investigation of Stator Seal Leakage on Aerodynamic Performance of Multistage Compressor

open access: yesFrontiers in Energy Research, 2021
In this paper, a numerical model based on the mass flow rate of seal leakage is presented, and a 3D numerical method of a multistage axial compressor with good engineering practicability is established.
Qi Wang   +7 more
doaj   +1 more source

The Investigation of the Stability for Multistage Axial Compressors [PDF]

open access: yesVolume 1: Aircraft Engine; Turbomachinery, 1985
The “actuator-delay-volume” is used as a physical model for stages of compressors instead of “actuator-lumped volume” model to predict the stability of multistage compressors. The stall line of a multistage compressor is predicted with these two models respectively.
Wenlan Li, Diyi Tang, Mengzi Cong
openaire   +2 more sources

A throughflow-based optimization method for multi-stage axial compressor

open access: yesAIP Advances, 2021
A multi-objective optimization tool for multi-stage axial compressors is developed based on an automatically calibrated throughflow method. The Euler-based throughflow equations with blade force terms are solved using a time-marching finite volume method
Cancan Li, Jiaqi Luo, Zuoli Xiao
doaj   +1 more source

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