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    Gas Turbine Field Performance Determination: Sources of Uncertainties 

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 001:;page 155
    Author(s): M. Pinelli; P. R. Spina
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an analysis of the uncertainties in the determination of gas turbine health, which arise by using a method of gas path analysis. This method uses field measurements to ...
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    A Multistage Compressor Test Facility: Uncertainty Analysis and Preliminary Test Results 

    Source: Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 001:;page 170
    Author(s): R. Bettocchi; P. R. Spina; M. Pinelli
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A multistage compressor test facility, fully instrumented with a dedicated data acquisition and processing system, has been developed to conduct experimental research work at the University of ...
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    A Feasibility Study of Existing Gas Turbines for Recuperated, Intercooled, and Reheat Cycle 

    Source: Journal of Engineering for Gas Turbines and Power:;2004:;volume( 126 ):;issue: 003:;page 531
    Author(s): R. Bhargava; M. Bianchi; A. Peretto; P. R. Spina
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the present paper, a comprehensive and simple in application design methodology to obtain a gas turbine working on recuperated, intercooled, and reheat cycle utilizing existing gas turbines ...
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    Influence of Blade Deterioration on Compressor and Turbine Performance 

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 003:;page 32401
    Author(s): M. Morini; M. Pinelli; P. R. Spina; M. Venturini
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gas turbine operating state determination consists of the assessment of the modification due to deterioration and fault of performance and geometric data characterizing machine components. One of ...
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    Artificial Intelligence for the Diagnostics of Gas Turbines—Part I: Neural Network Approach 

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 003:;page 711
    Author(s): R. Bettocchi; M. Pinelli; P. R. Spina; M. Venturini
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the paper, neural network (NN) models for gas turbine diagnostics are studied and developed. The analyses carried out are aimed at the selection of the most appropriate NN structure for ...
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    Artificial Intelligence for the Diagnostics of Gas Turbines—Part II: Neuro-Fuzzy Approach 

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 003:;page 720
    Author(s): R. Bettocchi; M. Pinelli; P. R. Spina; M. Venturini
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the paper, neuro-fuzzy systems (NFSs) for gas turbine diagnostics are studied and developed. The same procedure used previously for the setup of neural network (NN) models (, , , and , ...
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    Development and Validation of a Computational Code for Wet Compression Simulation of Gas Turbines 

    Source: Journal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 001:;page 12004
    Author(s): M. Bagnoli; P. R. Spina; M. Bianchi; F. Melino
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, a calculation code, developed in house by the authors, able to evaluate the performance of a gas turbine with all possible fogging strategies (high pressure fogging, overspray, ...
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    Erratum: “Influence of Blade Deterioration on Compressor and Turbine Performance” [Journal of Engineering for Gas Turbines and Power, 2010, 132(3), p. 032401] 

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 011:;page 117001
    Author(s): M. Morini; M. Pinelli; P. R. Spina; M. Venturini
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The correct form of the equation which defines ηC (reported on p. 10, first column, line 2 of the printed version) is the following:ηC=h(T0(n+1)s)−h(T01)h(T0(n+1))−h(T01)
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    Energy and Economic Analyses of Integrated Biogas-Fed Energy Systems 

    Source: Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 006:;page 61401
    Author(s): R. Bettocchi; M. Cadorin; G. Cenci; M. Morini; M. Pinelli; P. R. Spina; M. Venturini
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The process, which includes production, collection, carriage, and transformation of biomass into renewable fuels and then into energy (both electrical and thermal), involves a large number of ...
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    Setup of an Experimental Facility for the Investigation of Wet Compression on a Multistage Compressor 

    Source: Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 010:;page 102001
    Author(s): R. Bettocchi; G. Torsello; M. Morini; M. Pinelli; P. R. Spina; M. Venturini
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: At present, inlet fogging and wet compression are two of the most widely used approaches to enhance gas turbine performance, especially during hot seasons. However, potentially negative effects ...
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