The development of two experimental burners was completed as part of a project to evaluate the suitability of the use of converted reciprocating engine turbochargers as expendable jet engines for remotely piloted vehicles. As a result of analytic studies, Burner 'A' was constructed as a reverse flow burner and was designed to accept a mass flow up to 0.75 lbm/sec. Burner 'B' was also reverse and designed for a mass flow up to 1.5 lbm/sec. Both burners operated successfully on their respective turbochargers.


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    Titel :

    Combustor design for low cost expendable turbojets


    Weitere Titelangaben:

    Auslegung der Brennduesen fuer unaufwendige Strahltriebwerke


    Beteiligte:
    Greene, R.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1976


    Format / Umfang :

    56 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




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