Accession Number : ADA328006
Title : An Investigation into Computer Simulation of the Dynamic Response of a Gas Turbine Engine.
Descriptive Note : Master thesis,
Corporate Author : PENNSYLVANIA STATE UNIV UNIVERSITY PARK DEPT OF MECHANICAL ENGINEERING
Personal Author(s) : Henricks, Todd B.
PDF Url : ADA328006
Report Date : JUL 1997
Pagination or Media Count : 52
Abstract : Transient performance of gas turbines has a strong bearing on output and component life. For this reason, several articles have been written on the dynamic simulation of gas turbine systems in electrical generation, cogeneration, and marine applications. These models provide a basis for this present work. This paper describes a mathematical and computer model that was developed to investigate the dynamic response of a simple (no reheat, regeneration, or other auxiliary equipment) single-shaft gas turbine system. The model uses design parameters normally incorporated in gas turbine design (e.g. load coefficient, flow coefficient, and deHaller Number) as well as compressor and turbine stage geometry and compressor and turbine material properties. Also incorporated is a combustion chamber model. Other input parameters are included to enable the model to be adaptable to various system sizes and environments.
Descriptors : *COMPUTERIZED SIMULATION, *GAS TURBINES, MATHEMATICAL MODELS, INPUT, OUTPUT, TRANSIENTS, PERFORMANCE(ENGINEERING), DYNAMIC RESPONSE, THESES, COMBUSTION CHAMBERS, GEOMETRY, ELECTRIC POWER PRODUCTION, FLOW, COMPRESSORS.
Subject Categories : Computer Programming and Software
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE