Abstract We consider a turbofan engine (TFE), where the turbine rotor blades of the low pressure turbine (LPT) are micro-Laval nozzles. We demonstrated the possibility of integrating the super jet turbine and a jet nozzle as a single binary system for the purpose of generation of powerful coherence radiation. We estimated the efficiency of the binary high pressure emitting system being a TFE part.


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    Title :

    Study of performance of the aircraft gas turbine engine integrated with a gas dynamic laser


    Contributors:

    Published in:

    Russian Aeronautics ; 60 , 3 ; 474-477


    Publication date :

    2017-07-01


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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