Fundamental preliminary design considerations involved in integration are considered in terms 1965 and past technology; U S Army's XV-5A lift-fan research vehicle is used as basis of reference; lift-fan mechanical configuration is duscussed; parameters relating lift-fan static lift to power output of turbojet engine in terms of gas horsepower and gas flow output are established showing effects of three higher energy turbojet cycles on parameters; effects of higher energy turbojet gas generator on composite lift-fan propulsion system are also shown; it is found that 1965 technology can reduce propulsion weight of XV-5A by about 34%.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Lift-fan V/STOL propulsion and airframe integration


    Weitere Titelangaben:

    Aerodynamics Power Plant Installation -- 2 -- AGARDograph


    Beteiligte:
    Dickard, H.E. (Autor:in)


    Erscheinungsdatum :

    1965


    Format / Umfang :

    36 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Propulsion airframe integration

    Mikkelson, D. | NTRS | 1975



    Transonic Airframe Propulsion Integration

    R. E. Coltrin / B. W. Sanders / D. P. Bencze | NTIS | 1992


    LIFT RATINGS OF V/STOL PROPULSION UNITS

    Smith, E. G. / Thomas, W. W. | SAE Technical Papers | 1971


    Transonic airframe propulsion integration

    Coltrin, Robert E. / Sanders, Bobby W. / Bencze, Daniel P. | NTRS | 1992