Rocket engine thrust is the main performance parameters. The flow field of missile fight in different Mach is simulated by using FLUENT, then calculating the thrust of different conditions. The calculating results are consistent with the theory of Mach almost no effect on the thrust.


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    Titel :

    Study on the Impact of Missile Flight Mach to its Engine Thrust



    Erschienen in:

    Advanced Materials Research ; 1030-1032 ; 1331-1336


    Erscheinungsdatum :

    2014-09-22


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch







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