Pivot point concepts for fighter type aircraft with variable sweep wings are reviewed; vertical pin pivot configuration usually provides lightest structural arrangement; spanwise pivot point location is compromise between aerodynamic considerations and structural weight variations; aerodynamic considerations are usually most influential in overall optimization; Teflon lined journal bearings look very promising for sweep load spectra anticipated for fighter aircraft; service life of variable sweep fighter aircraft can be substantially increased by selecting aft sweep position for maximum possible usage.


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    Titel :

    Structural considerations for variable sweep wings


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Harvey, J.W. (Autor:in)

    Kongress:

    SAE Meeting ; 1967 Fighter



    Erscheinungsdatum :

    1967


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Structural Considerations for Variable Sweep Wings

    Harvey, J. W. | SAE Technical Papers | 1967


    Aircraft with Variable-Sweep Wings

    Page, R.K. | Emerald Group Publishing | 1965


    Aircraft with variable-sweep wings

    Page, R.K. | Engineering Index Backfile | 1965



    Mechanical Aspects of Variable Sweep Wings

    Paget, F. M. | SAE Technical Papers | 1967