The concept of a combined V/STOL propulsion and aircraft attitude control system was subjected to large scale engine tests. The tilt nacelle/attitude control vane package consisted of the T55 powered Hamilton Standard Q-Fan demonstrator. Vane forces, moments, thermal and acoustic characteristics as well as the effects on propulsion system performance were measured under conditions simulating hover in and out of ground effect.


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    Titel :

    Large Scale Static Tests of a Tilt-Nacelle V/STOL Propulsion/Attitude Control System


    Erscheinungsdatum :

    1978


    Format / Umfang :

    166 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch