Configurations considered are -- variable sweep wing; fixed wing, tail aft, 4 nacelles mounted on wing; fixed wing, canard Delta, trailing edge swept back 10°, leading edge swept back 60°, titanium wing and fuselage; fixed wing, canard Delta, trailing edge 0 °, leading edge 65°, steel wing and titanium fuselage; aerothermoelastic effects of sweep angle, wing thickness, "lg" working stress, and materials are shown; general considerations, such as probability predictions of survival of major structural component, fatigue spectrum considerations and estimations of magnitude of creep from 30,000 hr SST spectrum.


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    Titel :

    Design considerations for supersonic transport


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Fischler, J.E. (Autor:in)

    Kongress:

    SAE Meeting ; 1963 Supersonic



    Erscheinungsdatum :

    1963


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Design Considerations for a Supersonic Transport

    Fischler, J. E. | SAE Technical Papers | 1964


    SUPERSONIC TRANSPORT DEVELOPMENT CONSIDERATIONS

    FOSS, RICHARD L. | SAE Technical Papers | 1975


    Design considerations for supersonic transport electric power system

    Mintz, R.A. / Jessee, R.D. | Engineering Index Backfile | 1963


    Noise considerations in design and operation of supersonic transport

    Hubbard, H.H. / Maglieri, D.J. | Engineering Index Backfile | 1961


    Design Considerations for the Supersonic Transport Electric Power System

    Mintz, R. A. / Jessee, R. D. | SAE Technical Papers | 1963