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    Comparison Between the Steady Performance of Double Entry and Twin Entry Turbocharger Turbines 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 001:;page 11042
    Author(s): Romagnoli, Alessandro; Copeland, Colin D.; Martinez; Seiler, Martin; Rajoo, Srithar; Costall, Aaron
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Most boosting systems in internal combustion engines utilize “pulse turbochargingâ€‌ to maximize the energy extraction by the turbine. An internal combustion engine with more than four cylinders has a significant overlap ...
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    Effect of Exit Pressure Pulsation on the Performance and Stability Limit of a Turbocharger Centrifugal Compressor 

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 005:;page 52601
    Author(s): Barrera-Medrano, Maria Esperanza; Newton, Peter; Martinez-Botas, Ricardo; Rajoo, Srithar; Tomita, Isao; Ibaraki, Seiichi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is well known that compressor surge imposes a significant limit on the flow range of a turbocharged internal combustion engine. The centrifugal compressor is commonly placed upstream of the inlet manifold, and hence, ...
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    Optimization of an Organic Ranking Cycle Radial Turbine Using a Reduced-Order Model Coupled With Computational Fluid Dynamics 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 010:;page 101012
    Author(s): Alvarez-Regueiro, Eva;Yang, Bijie;Barrera-Medrano, Esperanza;Martinez-Botas, Ricardo;Rajoo, Srithar
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the geometry optimization of a single stage radial turbine for an organic ranking cycle (ORC) system operating over a pressure ratio of 9. The specific fluid used in this investigation is R1233zd (E), ...
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