All aircraft gas turbine engines currently compromise compression system performance at some point(s) in their operating envelope to obtain 'adequate' stall margin. This work pursues the concept of active stall control to minirnize or eliminate this penalty, thereby improving the performance of any aircraft gas turbine engine.


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    Title :

    Characterization of Stall Inception in High-Speed Single-Stage Compressors


    Contributors:
    K. Boyer (author)

    Publication date :

    1994


    Size :

    166 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Experimental and Theoretical Investigations of Stall Inception in a High-Speed Multi-Stage Compressors

    Escuret, J. F. / Garnier, V. / International Society for Air Breathing Engines; Australian Committee | British Library Conference Proceedings | 1995