A comparative evaluation of fixed-geometry and variable-sweep wing designs, a fixed delta wing, and oblique wings with a single body or two bodies suggests that an oblique wing is preferable in a transonic transport aircraft in terms of gross weight, fuel consumption, and aircraft noise, and also shows an acceptable aeroelastic stability. Further studies are, however, needed to develop the full potential of the oblique-wing concept, including its economic implications.


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    Titel :

    Transonic transport wings - Oblique or swept


    Beteiligte:
    Jones, R. T. (Autor:in) / Nisbet, J. W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1974-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Transonic transport wings - Oblique or swept

    Jones, R. T. / Nisbet, J. W. | NTRS | 1974


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