[go: up one dir, main page]

Miner, 2001 - Google Patents

3‐D Viscous Flow Analysis of a Mixed Flow Pump Impeller

Miner, 2001

View PDF
Document ID
15925409153036252949
Author
Miner S
Publication year
Publication venue
International Journal of Rotating Machinery

External Links

Snippet

This paper presents the results of a study using a coarse grid to analyze the flow in the impeller of a mixed flow pump. A commercial computational fluid dynamics code (FLOTRAN) is used to solve the 3‐D Reynolds Averaged Navier Stokes equations in a rotating …
Continue reading at onlinelibrary.wiley.com (PDF) (other versions)

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F04—POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or anti-vibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F04—POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing

Similar Documents

Publication Publication Date Title
Denton The calculation of three-dimensional viscous flow through multistage turbomachines
El-Naggar A One‐Dimensional Flow Analysis for the Prediction of Centrifugal Pump Performance Characteristics
Campobasso et al. Effects of flow instabilities on the linear analysis of turbomachinery aeroelasticity
Miyazawa et al. Unsteady force on multi-stage and multi-passage turbine long blade rows induced by wet-steam flows
Shukla et al. Numerical experiments on a centrifugal pump
Miner 3‐D Viscous Flow Analysis of a Mixed Flow Pump Impeller
Schweitzer et al. Computational fluid dynamics in torque converters: validation and application
Miner Evaluation of blade passage analysis using coarse grids
Peeters et al. A numerical investigation of the unsteady flow in centrifugal stages
Miner CFD Analysis of the First‐Stage Rotor and Stator in a Two‐Stage Mixed Flow Pump
Valentini et al. Experimental validation of a reduced order for radial turbopump design
Van den Braembussche et al. Design and optimization of a multistage turbine for helium cooled reactor
Balsa et al. The simulation of axial compressor performance using an annulus wall boundary layer theory
Thompson Fluid dynamic excitation of centrifugal compressor rotor vibrations
Fukaya et al. Prediction of cavitation performance of axial flow pump by using numerical cavitating flow simulation with bubble flow model
Tokuyama et al. Computational analysis of unsteady flow in a partial admission supersonic turbine stage
Miner 3‐D Viscous Flow Analysis of an Axial Flow Pump Impeller
Ye et al. Effects of the shock wave structure on the tip clearance leakage flow in transonic compressor rotors
Rosa et al. CFD simulation of a centrifugal pump impeller with variations of number of blades
Dunham Modelling of spanwise mixing in compressor through-flow computations
Sato et al. Numerical investigation into the effects of a radial gap on hydraulic turbine performance
Shukla et al. Numerical prediction of NPSHR characteristics of double suction centrifugal pump
Griffin et al. Analytical Investigation of the Unsteady Aerodynamic Environments in Space Shuttle Main Engine (SSME) Turbines
Dalbanjan et al. Effect of Rotor Tip and Stator Hub Clearance on Aero Performance in Axial Flow Compressors for Aero Gas Turbine Engines
Rahmati Application of a pressure correction method for modeling incompressible flow through turbomachines