Results 1 to 10 of about 8,509 (316)
Numerical study of probe parameters on performance of a transonic axial compressor. [PDF]
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]
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]
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
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
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
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
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
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]
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]
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

