The advancement of technology in gas turbine engines used for aerospace propulsion has been focused on achieving significant performance improvements. At the system level, these improvements are expressed in metrics such as engine thrust-to-weight ratio and system and component efficiencies. The overall goals are directed at reducing engine weight, fuel burn, emissions, and noise. At a component level, these goals translate into aggressive designs of each engine component well beyond the state of the art.


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    Title :

    Flow Control Opportunities for Propulsion Systems


    Contributors:

    Publication date :

    2008-06-23


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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