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    The Role of the Working Fluid and Nonideal Thermodynamic Effects on Performance of Gas-Lubricated Bearings 

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 006:;page 61015-1
    Author(s): de Waart, Wessel; Pini, Matteo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Small-scale turbomachinery operating at high rotational speed is a key technology for increasing the power density of energy and propulsion systems. A notable example is the turbine of an organic Rankine cycle turbogenerator ...
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    Design Guidelines for Axial Turbines Operating With Non-Ideal Compressible Flows 

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 143 ):;issue: 001:;page 011004-1
    Author(s): Giuffre', Andrea; Pini, Matteo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The impact of non-ideal compressible flows on the fluid-dynamic design of axial turbine stages is examined. First, the classical similarity equation (CSE) is revised and extended to account for the effect of flow non-ideality. ...
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    A Review of Numerical Methodologies for Predicting Rotating Stall and Surge in High-Speed Centrifugal Compressors 

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 004:;page 40801-1
    Author(s): Neri, Francesco; Hickel, Stefan; Pini, Matteo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High-speed supersonic radial compressors are a critical enabling technology for meeting the requirements of future aviation-propulsion and thermal-management systems. These turbomachines must be designed to be both efficient ...
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    Design Optimization of a High-Speed Twin-Stage Compressor for Next-Gen Aircraft Environmental Control System 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 145 ):;issue: 003:;page 31017-1
    Author(s): Giuffre', Andrea; Colonna, Piero; Pini, Matteo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The environmental control system (ECS) is the largest auxiliary power consumer, i.e., around 75% of non-propulsive power, among the aircraft subsystems. The adoption of a novel ECS architecture, based on an electrically-driven ...
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    Multirow Adjoint-Based Optimization of NICFD Turbomachinery Using a Computer-Aided Design-Based Parametrization 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 004:;page 41008-1
    Author(s): Agromayor, Roberto; Anand, Nitish; Pini, Matteo; Nord, Lars O.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Currently, most of the adjoint-based design systems documented in the open literature assume that the fluid behaves as an ideal gas, are restricted to the optimization of a single row of blades, or are not suited to impose ...
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    A Code for the Preliminary Design of Cooled Supercritical CO2 Turbines and Application to the Allam Cycle 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 003:;page 31012-1
    Author(s): Scaccabarozzi, Roberto; Martelli, Emanuele; Pini, Matteo; De Servi, Carlo Maria; Chiesa, Paolo; Gatti, Manuele
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper documents a thermo-fluid-dynamic mean-line model for the preliminary design of multistage axial turbines with blade cooling applicable to supercritical CO2 turbines. Given the working fluid and coolant inlet ...
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    Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 003:;page 31014-1
    Author(s): Mushtaq, Noraiz; Pini, Matteo; Gaetani, Paolo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A supersonic inlet turbine can extract substantial energy from the highly fluctuating and transonic flow delivered by a rotating detonation combustor (RDC). However, a transition duct is necessary to achieve the supersonic ...
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    Centrifugal Turbines for Mini Organic Rankine Cycle Power Systems 

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 012:;page 122607
    Author(s): Casati, Emiliano; Vitale, Salvatore; Pini, Matteo; Persico, Giacomo; Colonna, Piero
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Organic Rankine cycle (ORC) power systems are rapidly diffusing as a technology for the conversion of thermal energy sources in the smalltomedium power range, e.g., from 150 kWe up to several MWe. The most critical component ...
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    Aerodynamics of Centrifugal Turbine Cascades 

    Source: Journal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 011:;page 112602
    Author(s): Persico, Giacomo; Pini, Matteo; Dossena, Vincenzo; Gaetani, Paolo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The centrifugal turbine architecture is a promising solution for smalltomedium organic Rankine cycle (ORC) power systems. The inherent compactness of the multistage arrangement makes this configuration very attractive for ...
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    Design, Simulation, and Construction of a Test Rig for Organic Vapors 

    Source: Journal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 004:;page 42304
    Author(s): Spinelli, Andrea; Pini, Matteo; Dossena, Vincenzo; Gaetani, Paolo; Casella, Francesco
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A blowdown wind tunnel for realgas applications has been designed, validated by means of dynamic simulation, and then built. The facility is aimed at characterizing an organic vapor stream, representative of the expansion ...
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