This paper presents an analysis of the mechanism of compressor surge in a turbo-jet engine due to pressure disturbances at the air intake inlet. The computational model simulating the whole engine from the air intake to the exhaust nozzle, can predict surge hammer, as well as compressor surge cycles. The computed results show that a significant correlation exists between the compressor surge and the magnitude and duration of the pressure disturbances. (DePo)


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    Title :

    A study on the mechanism of compressor surge due to inlet pressure disturbances


    Additional title:

    Studie des Mechanismuses von Verdichterstoerungen durch Stoerungen im Einlassdruck


    Contributors:
    Sugiyama, Y. (author) / Hamed, A. (author) / Iabakoff, W. (author)

    Published in:

    Publication date :

    1978


    Size :

    11 Seiten, 16 Bilder, 17 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English