[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Zhao et al., 2020 - Google Patents

Investigation of variable orifice plate design for centrifugal compressor low-end performance improvement

Zhao et al., 2020

Document ID
7116702689779791582
Author
Zhao B
Hu L
Zhao Q
Zhou X
Publication year
Publication venue
Aerospace Science and Technology

External Links

Snippet

In the present paper, a compressor with variable inlet configuration upstream of the compressor wheel was investigated to improve the compressor low-end performance. As a concept study, the variable inlet configuration was assumed to be a variable orifice plate …
Continue reading at www.sciencedirect.com (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation

Similar Documents

Publication Publication Date Title
Zhao et al. Investigation of variable orifice plate design for centrifugal compressor low-end performance improvement
Spakovszky et al. Spike and modal stall inception in an advanced turbocharger centrifugal compressor
Jiao et al. Numerical simulation of air flow through turbocharger compressors with dual volute design
Xu et al. Empirical design considerations for industrial centrifugal compressors
Chen et al. Casing treatment and inlet swirl of centrifugal compressors
Jung et al. Effect of tip clearance, winglets, and shroud height on the tip leakage in axial flow fans
Yang et al. Investigation of stall process flow field in transonic centrifugal compressor with volute
Hellstrom et al. Large eddy simulation of the unsteady flow in a radial compressor operating near surge
Sivagnanasundaram et al. Map width enhancement technique for a turbocharger compressor
Hu et al. Stability and structural sensitivity analysis of the turbulent flow in the narrow vaneless diffuser with mean flow method
Dehner et al. Simulation of deep surge in a turbocharger compression system
Wang et al. Coupling method of stability enhancement based on casing treatments in an axial compressor
Zheng et al. Stability improvement of a turbocharger centrifugal compressor by a nonaxisymmetric vaned diffuser
Huang et al. Compressor surge based on a 1D-3D coupled method–Part 2: Surge investigation
Dehner et al. Three-dimensional computational fluid dynamics prediction of turbocharger centrifugal compression system instabilities
Xu et al. Effects of asymmetric radial clearance on performance of a centrifugal compressor
Zhang et al. Inlet bent torsional pipe effect on the performance and stability of a centrifugal compressor with volute
Wang et al. Failure mechanism of casing treatment in improving stability of a highly loaded two-stage axial compressor
Chen et al. Pressure drop analysis and aerodynamic design of compressor L-inlet duct
Mansouri et al. Heat transfer characteristics of a high-pressure turbine under combined distorted hot-streak and residual swirl: an unsteady computational study
Lin et al. Roles of recirculating bubble on the performance of centrifugal compressors
Ding et al. Flow mechanism of self-recirculating casing treatment in a low-reaction transonic compressor rotor
Zhao et al. Investigation of using multi-shockwave system instead of single normal shock for improving radial inflow turbine reliability
Zhang et al. Numerical investigation on the flow and heat transfer characteristics in radial pre-swirl system with different fillet radius at the junction of inlet cavity and nozzle
Ryu et al. Numerical and experimental investigation into effects of winglet shape on flow and noise performances of axial-flow fans for outdoor unit of air conditioner