Abstract A system of differential equations of the variable-mass body spatial motion was solved on the basis of a modern technique for calculating aerodynamic coefficients and inertial-mass characteristics of aircraft. The best working parameters of a jet engine were chosen to increase the flight range on retention of the optimal jet engine dimensions.


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    Titel :

    Choice of working parameters of a solid-fuel jet engine of unguided aircraft


    Beteiligte:
    Makeev, V. I. (Autor:in) / Pushkarev, Yu. I. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2013-10-01


    Format / Umfang :

    10 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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