An analysis was made of the flow redistribution which occurs at the exit of an inlet due to the presence of a compressor. The flow redistribution includes a change in the axial velocity distortion, which is a function of the slope of the curve of compressor pressure coefficient versus flow coefficient at a particular corrected speed. (Author)


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    Title :

    A Problem in Matching an Inlet and Engine Having Steady-State Circumferential Inlet Pressure Distortion


    Contributors:

    Publication date :

    1970


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English