Numerical Investigation of the Effect of Different Back Sweep Angle and Exducer Width on the Impeller Outlet Flow Pattern of a Centrifugal Compressor With Vaneless Diffuser

Author:

Hildebrandt A.1,Genrup M.1

Affiliation:

1. LTH, Lund Institute of Technology, Department of Energy Sciences, P.O. Box 118, 22100 Lund, Sweden

Abstract

This paper presents a numerical investigation of the effect of different back sweep angles and exducer widths on the steady-state impeller outlet flow pattern of a centrifugal compressor with a vaneless diffuser. The investigations have been performed with commercial computational fluid dynamics (CFD) and in-house programmed one-dimensional (1D) codes. CFD calculations aim to investigate how flow pattern from the impeller is quantitatively influenced by compressor geometry parameters; thereby, the location of wake and its magnitude (flow angle and relative velocity magnitude) are analyzed. Results show that the increased back sweep impeller provides a more uniform flow pattern in terms of velocity and flow deviation angle distribution, and offers better potential for the diffusion process inside a vaneless (or vaned) diffuser. Secondary flux fraction and flow deviation angle from CFD simulation are implemented into the 1D two-zone program to improve 1D prediction results.

Publisher

ASME International

Subject

Mechanical Engineering

Reference15 articles.

1. Investigation of an Inversely Designed Centrifugal Compressor Stage—Part 1: Design and Numerical Verification;Zangeneh;ASME J. Turbomach.

2. Unsteady-Diffuser Flow in a Transonic Centrifugal Compressor;Krain;Int. J. Rotating Mach.

3. Analysis of Secondary Flows in Centrifugal Impellers

4. Ziegler, K. U. , 2003, “Experimentelle Untersuchung der Laufrad-Diffuser-Interaktion in einem Radialverdichter variabler Geometrie,” (Dissertation RWTH Aachen), Shaker Verlag, Germany, Aachen, D82.

5. Instantaneous Measurements in the Jet-Wake Discharge Flow of a Centrifugal Compressor Impeller;Eckardt;ASME J. Eng. Power

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