The results of a detailed preliminary design study of a V/STOL research test vehicle (RTV), employing ARL thrust augmentation concepts, are presented. The V/STOL research airplane uses a high by-pass ratio turbofan engine with ejector thrust augmentation in the wing and fuselage nose. Design layouts of all major configuration components and systems are presented together with results of analytical investigations and trade-off studies.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    V/STOL Employing ARL Thrust Augmentation Concepts - Research Test Vehicle Configuration Summary and Design Technology Report


    Beteiligte:
    C. Henderson (Autor:in)

    Erscheinungsdatum :

    1968


    Format / Umfang :

    434 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch