This report presents a review of current compressor blade-element theory with particular emphasis on application to the transonic high-performance compressor. A discussion of the significant parameters of total-pressure loss and deviation angle is presented, and an indication of the extent of available knowledge and the problems involved in the determination of blade-element characteristics is given. Some recent results and considerations in this pursuit and suggestions for further avenues of investigation are indicated.


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    Title :

    Review of high-performance axial-flow-compressor blade-element theory


    Contributors:

    Publication date :

    1954-04-06


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English