Flight control studies conducted during the STOL Tactical Aircraft Investigation by Convair Aerospace were directed toward development of flight control systems for three versions of the medium STOL transport. Baseline vehicles used for flight control studies were: externally blown flap, internally blown flap, and mechanical flap/vectored thrust configurations. Requirements of MIL-F-8785B and MIL-F-833000 for aircraft handling qualities were the guiding criteria for the control system study. The mechanization trade study concluded that fly-by-wire mechanization is preferred over the more mechanical version which requires significant fly-by-wire features to achieve the required augmentation and decoupling. (Modified author abstract)


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    Titel :

    STOL Tactical Aircraft Investigation. Volume V. Flight Control Technology


    Beteiligte:
    J. Hebert (Autor:in) / G. Campbell (Autor:in) / E. Price (Autor:in) / L. B. White (Autor:in) / R. Halstenberg (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    358 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    STOL Tactical Aircraft Investigation

    Hebert, Joseph | SAE Technical Papers | 1973


    STOL Tactical Aircraft Investigation. Volume I. Configuration Definition

    J. Hebert / C. Whitney / R. E. Johnston et al. | NTIS | 1973



    JET V/STOL TACTICAL AIRCRAFT

    Alford, W. J., Jr. / Kuhn, R. E. / Reeder, J. P. | NTRS | 1963


    Jet V/STOL tactical aircraft

    Kuhn, R.E. / Reeder, J.P. / Alford, Jr., W.J. | Engineering Index Backfile | 1963