The results of a general VTOL airplane ground effect investigation for one to four lifting turbojets installed in the fuselage and wings are presented in this paper. The study provides information that will be very useful in the preliminary design layout and evaluation phase of VTOL development. The tests described here were conducted in Bell Aerosystems jet impingement test facility, which utilizes plant compressed air to provide model exhaust gas flows and a steam ejector to induce inlet flow equal to the exhaust flow. The model simulates a 20,000 lb class aircraft at about 1:10 scale.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Studies of VTOL Inlet Temperature Rise and Lift-Thrust


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Sherman, E. W. (Autor:in)

    Kongress:

    SAE World Congress & Exhibition ; 1964



    Erscheinungsdatum :

    1964-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Lift/thrust engines for VTOL aircraft

    Engineering Index Backfile | 1961


    Separated lift-thrust VTOL aircraft with articulated rotors

    BAITY SEAN MARSHALL / MILLER STEPHEN W | Europäisches Patentamt | 2024

    Freier Zugriff

    SEPARATED LIFT-THRUST VTOL AIRCRAFT WITH ARTICULATED ROTORS

    BAITY SEAN MARSHALL / MILLER STEPHEN W | Europäisches Patentamt | 2021

    Freier Zugriff

    Separated lift-thrust VTOL aircraft with articulated rotors

    BAITY SEAN MARSHALL / MILLER STEPHEN W | Europäisches Patentamt | 2024

    Freier Zugriff

    SEPARATED LIFT-THRUST VTOL AIRCRAFT WITH ARTICULATED ROTORS

    BAITY SEAN MARSHALL / MILLER STEPHEN W | Europäisches Patentamt | 2022

    Freier Zugriff