Multi-quadrant performance simulation for subsonic axial flow compressors / Werner van Antwerpen

The emergence of closed-loop Brayton cycle power plants, such as the PBMR, resulted in the need to simulate start-up transients for industrial multi-stage axial flow compressors operating at subsonic conditions. This implies that the delivery pressure and power requirements must be predicted for dif...

Full description

Bibliographic Details
Main Author: Van Antwerpen, Werner
Published: North-West University 2009
Subjects:
Online Access:http://hdl.handle.net/10394/1271
id ndltd-NWUBOLOKA1-oai-dspace.nwu.ac.za-10394-1271
record_format oai_dc
spelling ndltd-NWUBOLOKA1-oai-dspace.nwu.ac.za-10394-12712014-04-16T03:55:25ZMulti-quadrant performance simulation for subsonic axial flow compressors / Werner van AntwerpenVan Antwerpen, WernerLossAxial flow compressorQuadrantSubsonicMean-lineStart-upSimulationThe emergence of closed-loop Brayton cycle power plants, such as the PBMR, resulted in the need to simulate start-up transients for industrial multi-stage axial flow compressors operating at subsonic conditions. This implies that the delivery pressure and power requirements must be predicted for different mass flow rates and rotational speeds while operating in the first and fourth quadrants on the compressor performance charts. Therefore, an analytical performance prediction model for subsonic multi-stage axial flow compressors had to be developed that can be integrated into a generic network analysis software code such as Flownex. For this purpose, performance calculations based on one-dimensional mean-line analysis demonstrated good accuracy, provided that the correct models for losses, incidence and deviation are used. Such a model is therefore the focus of this study. A preliminary analytical performance prediction code, with the capability of interchanging between different deviation and loss models is presented. Reasonably complex loss models are integrated in association with the correct incidence and deviation models in a software package called "Engineering Equation Solver" (EES). The total pressure loss calculations are based on a superposition of theoretically separable loss components that include the following: blade profile losses, secondary losses and annulus losses. The fundamental conservation equations for mass, momentum and energy for compressible "rotating pipe" flow were implemented into the performance prediction code. Performance prediction models were validated against experimental data and evaluated according to their ease of implementation. Verification was done by comparing simulation results with experimental work done by Von Backstrom. This includes a calculation to determine the uncertainty in the experimental results. Furthermore, since the conventional definition of isentropic efficiency breaks down at the boundaries of quadrants on the performance charts, a new non-dimensional power formulation is presented that allows for the calculation of the compressor power in all of the relevant quadrants. Good comparison was found between simulation results and measurements in the first and fourth quadrant of operation.Thesis (M.Ing. (Nuclear Engineering))--North-West University, Potchefstroom Campus, 2007.North-West University2009-03-02T15:19:39Z2009-03-02T15:19:39Z2007Thesishttp://hdl.handle.net/10394/1271
collection NDLTD
sources NDLTD
topic Loss
Axial flow compressor
Quadrant
Subsonic
Mean-line
Start-up
Simulation
spellingShingle Loss
Axial flow compressor
Quadrant
Subsonic
Mean-line
Start-up
Simulation
Van Antwerpen, Werner
Multi-quadrant performance simulation for subsonic axial flow compressors / Werner van Antwerpen
description The emergence of closed-loop Brayton cycle power plants, such as the PBMR, resulted in the need to simulate start-up transients for industrial multi-stage axial flow compressors operating at subsonic conditions. This implies that the delivery pressure and power requirements must be predicted for different mass flow rates and rotational speeds while operating in the first and fourth quadrants on the compressor performance charts. Therefore, an analytical performance prediction model for subsonic multi-stage axial flow compressors had to be developed that can be integrated into a generic network analysis software code such as Flownex. For this purpose, performance calculations based on one-dimensional mean-line analysis demonstrated good accuracy, provided that the correct models for losses, incidence and deviation are used. Such a model is therefore the focus of this study. A preliminary analytical performance prediction code, with the capability of interchanging between different deviation and loss models is presented. Reasonably complex loss models are integrated in association with the correct incidence and deviation models in a software package called "Engineering Equation Solver" (EES). The total pressure loss calculations are based on a superposition of theoretically separable loss components that include the following: blade profile losses, secondary losses and annulus losses. The fundamental conservation equations for mass, momentum and energy for compressible "rotating pipe" flow were implemented into the performance prediction code. Performance prediction models were validated against experimental data and evaluated according to their ease of implementation. Verification was done by comparing simulation results with experimental work done by Von Backstrom. This includes a calculation to determine the uncertainty in the experimental results. Furthermore, since the conventional definition of isentropic efficiency breaks down at the boundaries of quadrants on the performance charts, a new non-dimensional power formulation is presented that allows for the calculation of the compressor power in all of the relevant quadrants. Good comparison was found between simulation results and measurements in the first and fourth quadrant of operation. === Thesis (M.Ing. (Nuclear Engineering))--North-West University, Potchefstroom Campus, 2007.
author Van Antwerpen, Werner
author_facet Van Antwerpen, Werner
author_sort Van Antwerpen, Werner
title Multi-quadrant performance simulation for subsonic axial flow compressors / Werner van Antwerpen
title_short Multi-quadrant performance simulation for subsonic axial flow compressors / Werner van Antwerpen
title_full Multi-quadrant performance simulation for subsonic axial flow compressors / Werner van Antwerpen
title_fullStr Multi-quadrant performance simulation for subsonic axial flow compressors / Werner van Antwerpen
title_full_unstemmed Multi-quadrant performance simulation for subsonic axial flow compressors / Werner van Antwerpen
title_sort multi-quadrant performance simulation for subsonic axial flow compressors / werner van antwerpen
publisher North-West University
publishDate 2009
url http://hdl.handle.net/10394/1271
work_keys_str_mv AT vanantwerpenwerner multiquadrantperformancesimulationforsubsonicaxialflowcompressorswernervanantwerpen
_version_ 1716664468670251008