[HTML][HTML] Gas path fault and degradation modelling in twin-shaft gas turbines

S Cruz-Manzo, V Panov, Y Zhang - Machines, 2018 - mdpi.com
In this study, an assessment of degradation and failure modes in the gas-path components
of twin-shaft industrial gas turbines (IGTs) has been carried out through a model-based …

Analysis of performance of a twin-shaft gas turbine during hot-end damage in the gas generator turbine

S Cruz-Manzo, S Maleki… - … Expo: Power for …, 2018 - asmedigitalcollection.asme.org
In this study, an analysis of the performance of a twin-shaft industrial gas turbine (IGT) during
hot-end damage in the gas generator turbine (GGT) at high-power operation has been …

Inter-stage dynamic performance of an axial compressor of a twin-shaft industrial gas turbine

S Cruz-Manzo, S Krishnababu, V Panov, C Bingham - Machines, 2020 - mdpi.com
In this study, the inter-stage dynamic performance of a multistage axial compressor is
simulated through a semi-empirical model constructed in the Matlab Simulink environment …

Development of a steady-state thermodynamic model in microsoft excel for performance analysis of industrial gas turbines

TA Clifford, S Cruz-Manzo, Y Zhang… - IECON 2017-43rd …, 2017 - ieeexplore.ieee.org
In this paper, an off-design performance prediction model for a single shaft industrial gas
turbine (IGT) using Microsoft Excel with Visual Basic for Applications (VBA) programming is …

Calculation of the Overspeed at Emergency Shutdown of a Transonic Test Turbine Facility Using a Web-Based Thermodynamic Simulation Tool

W Sanz, E Perz, E Göttlich - … Expo: Power for …, 2024 - asmedigitalcollection.asme.org
Abstract The Institute of Thermal Turbomachinery and Machine Dynamics at Graz University
of Technology operates a Transonic Test Turbine Facility of 3 MW power. The test turbine is …

[PDF][PDF] Performance calculation of a multi-stage axial compressor through a semi-empirical modelling framework

S Cruz-Manzo, S Krishnababu, V Panov… - Proceedings of the …, 2019 - academia.edu
In this study, calculation of the performance of an axial compressor from a twin-shaft
industrial gas turbine (IGT) is carried out through a semi-empirical modelling framework. The …

PERFORMANCE CALCULATION OF A MULTI-STAGE AXIAL COMPRESSOR THROUGH A SEMI-EMPIRICAL MODELLING FRAMEWORK

S Krishnababu, S Cruz-Manzo, V Panov, Y Zhang - 2019 - repository.lincoln.ac.uk
In this study, calculation of the performance of an axial compressor from a twin-shaft
industrial gas turbine (IGT) is carried out through a semi-empirical modelling framework. The …

ANALYSIS OF PERFORMANCE OF A TWIN-SHAFT GAS TURBINE DURING HOT-END DAMAGE IN THE GAS GENERATOR TURBINE

F Agbonzikilo, S Cruz-Manzo, S Maleki, V Panov… - 2018 - repository.lincoln.ac.uk
In this study, an analysis of the performance of a twin-shaft industrial gas turbine (IGT) during
hot-end damage in the gas generator turbine (GGT) at high-power operation has been …

Development of a steady-state thermodynamic model in Microsoft Excel for performance analysis of industrial gas turbines

A Latimer, T Clifford, S Cruz-Manzo, V Panov, Y Zhang - 2017 - repository.lincoln.ac.uk
In this paper, an off-design performance prediction model for a single shaft industrial gas
turbine (IGT) using Microsoft Excel with Visual Basic for Applications (VBA) programming is …