Variable geometry aircraft greatly reduces design compromises normally made with fixed wing aircraft and allows significant increases in performance that otherwise might not be obtainable; major changes in flight characteristics due to variable wing sweep are longitudinal and these handling qualities can be improved with stability augmentation; aircraft ride qualities are greatly improved with aft wing sweep; trim change associated with wing sweep is not large and is compensated for by flight control system; augmented flight control system is desirable with variable geometry aircraft.


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    Titel :

    Pilot comments on variable geometry aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Parsons, R.K. (Autor:in)

    Kongress:

    SAE Meeting ; 1967 Design



    Erscheinungsdatum :

    1967


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Pilot Comments on Variable Geometry Aircraft

    Parsons, Major Robert K. | SAE Technical Papers | 1967


    Variable geometry for aircraft

    Cownie, J.R. | Engineering Index Backfile | 1958


    Problems of variable-geometry aircraft

    Heath, B.O. | Engineering Index Backfile | 1967


    Maintainability Considerations in Variable Geometry Aircraft

    Onewein, L. J. | SAE Technical Papers | 1967


    Variable geometry in supersonic transport aircraft

    Swihart, J.M. | Engineering Index Backfile | 1967