Results 1 to 10 of about 8,509 (316)

Numerical study of probe parameters on performance of a transonic axial compressor. [PDF]

open access: yesPLoS ONE, 2021
The paper shows the effect of the probe on the performance of a transonic axial speed compressor. The unobstructed flow case with the experimental data was validated and used as a guide for all subsequent study cases.
Asad Islam, Hongwei Ma
doaj   +2 more sources

Unsteady Deffuser Flow in a Transonic Centrifugal Compressor [PDF]

open access: yesInternational Journal of Rotating Machinery, 2002
The paper deals with the clarification of the unsteady, transonic flow phenomena occurring in the vaned diffuser area of a high pressure ratio centrifugal compressor stage. A description of the test rig, the measurement technique applied and a brief description of the steady 3D code used for the theoretical investigations are given.
Krain Hartmut
doaj   +6 more sources

Influence of Blade Lean on Performance and Shock Wave/Tip Leakage Flow Interaction in a Transonic Compressor Rotor [PDF]

open access: yesJournal of Applied Fluid Mechanics, 2022
Blade lean has been extensively used in axial compressor stators to control flow separations, but its influence mechanism on transonic compressor rotors remains to be revealed.
Z. Cao, X. Zhang, Y. Liang, B. Liu
doaj   +1 more source

Parametric Research and Aerodynamic Characteristic of a Two-Stage Transonic Compressor for a Turbine Based Combined Cycle Engine

open access: yesAerospace, 2022
This paper researches the parametric optimization of a two-stage transonic compressor having a large air bypass at partial rotating speed according to flow analysis for a turbine-based combined cycle engine (TBCC).
Hengtao Shi
doaj   +1 more source

Performance Improvement of a Highly Loaded Transonic Centrifugal Compressor with Tandem Impeller and Freeform Blade Configuration

open access: yesEnergies, 2022
A highly loaded transonic centrifugal compressor is aerodynamically designed and numerically investigated. The objectives are to improve the compressor efficiency by using tandem impeller configuration and 3D free-formed blade design concepts.
Ziliang Li, Yanhui Wu, Xingen Lu
doaj   +1 more source

Experimental Aerodynamic and Aeroelastic Investigation of a Transonic Compressor Rotor with Reduced Blade Count

open access: yesInternational Journal of Turbomachinery, Propulsion and Power, 2021
This study investigates the aerodynamic and aeroelastic characteristics of a transonic axial compressor, focusing on blade count reduced rotor behavior.
Daniel Franke   +5 more
doaj   +1 more source

Verification of a transonic stage CFD model for assessing the erosion wear influence on the operation of the axial compressor

open access: yesВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2023
The paper presents the results of one of the stages of creating a model of assessing and forecasting the operating characteristics of a transonic compressor due to erosive wear.
V. L. Blinov, I. S. Zubkov
doaj   +1 more source

Transient Analysis of Flow Unsteadiness and Noise Characteristics in a Centrifugal Compressor with a Novel Vaned Diffuser

open access: yesApplied Sciences, 2021
The demands to apply transonic centrifugal compressor have increased in the advanced gas turbine engines. Various techniques are used to increase the aerodynamic performance of the centrifugal compressor.
Ali Zamiri   +3 more
doaj   +1 more source

Transonic Relief in Fans and Compressors [PDF]

open access: yesVolume 2A: Turbomachinery, 2020
Abstract Every supersonic fan or compressor blade row has a streamtube, the ‘sonic streamtube’, which operates with a blade relative inlet Mach number of one. A key parameter in the design of the ‘sonic streamtube’ is the area ratio between the blade throat area and upstream passage area, Athroat/Ainlet.
Demetrios Lefas, Robert J. Miller
openaire   +1 more source

Aerodynamic instabilities in transonic centrifugal compressor [PDF]

open access: yesMechanics & Industry, 2014
This paper presents the analysis of the instabilities inception in a transonic centrifugal com-pressor for different rotation speeds. The analysis was conducted from experimental results obtained with unsteady pressure sensors implanted in the inducer, vaneless diffuser and vaned diffuser.
Buffaz, Nicolas, Trébinjac, Isabelle
openaire   +2 more sources

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