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    The Effect of Tip Leakage Vortex for Operating Range Enhancement of Centrifugal Compressor 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 005:;page 51020
    Author(s): Tomita, Isao; Ibaraki, Seiichi; Furukawa, Masato; Yamada, Kazutoyo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recently, the application of turbochargers is increasing because they are effective in improving fuel consumption of engines. One of the most important turbocharger characteristics is compressor operating range, since it ...
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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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    On the Effect of Engine Pulsations on the Performance of a Turbocharger Centrifugal Compressor 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 008:;page 81001
    Author(s): Barrera-Medrano, Maria Esperanza; Martinez-Botas, Ricardo; Tomita, Isao; Ibaraki, Seiichi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In an internal combustion engine, the centrifugal compressor is placed upstream of the inlet manifold and therefore, it is exposed an unsteady flow regime caused by the inlet valves of the cylinder arrangement. This valve ...
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