Wing pivot structure, which is key to United States supersonic transport, has been developed through one-quarter scale and full-scale tests, and complete wing pivot structure, including fixed inboard portion and movable outboard portion, is currently in test; Ti 6Al-4V alloy that has been selected for wing primary structure will meet 50,000 hr design life of airplane; with proper inspection and maintenance, fatigue life of this fail-safe structure can be extended indefinitely; direct lift control system, and supersonic inlet control system also discussed.


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    Titel :

    Variable geometry in supersonic transport aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Swihart, J.M. (Autor:in)

    Kongress:

    SAE Meeting ; 1967 Supersonic



    Erscheinungsdatum :

    1967


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Variable Geometry in a Supersonic Transport Aircraft

    Swihart, John M. | SAE Technical Papers | 1967


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    Antaran, Albert / Belete, Hailu / Dryzmkowski, Mark et al. | NTRS | 1992


    Supersonic transport aircraft

    Russell, A.E. | Engineering Index Backfile | 1962