In this paper, a procedure to obtain the compressor map (pressure ratio vs. mass flow rate) is showed by scaling of the available compressor maps with similar shape and design using scaling theorem. The reason to develop such procedure is that in industrial application, a new compressor map need be developed before the complete geometry and hardware of compressor are known. Such procedure is especially useful for users such as engine or vehicle OEM to quickly select turbocharger compressor independently. The scaling law is used to model the non-dimensional parameters of compressor head coefficient vs. mass flow coefficient. Detail procedure from the non-dimensional parameters to the final compressor performance data are described.


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    Title :

    Modeling Compressor Pressure Ratio vs. Mass Flow Rate Including Choke Line and Surge Line Using Scaling Theorem


    Additional title:

    Sae Technical Papers


    Contributors:
    Yang, Bo (author)

    Conference:

    AeroTech ; 2022



    Publication date :

    2022-03-08




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    AXIAL FLOW MULTISTAGE COMPRESSOR SURGE LINE DETERMINATION IN PERFORMING CALCULATION STUDIES

    Вадим Анатольевич Даценко / Александр Евгеньевич Дёмин / Наталия Владимировна Пижанкова | DOAJ | 2020

    Free access