The avoidance of sonic booms places a constraint on aircraft design and can lead to unusual new configurations. From a comparison among several candidate designs, it is shown that an oblique-wing aircraft offers many advantages when structure, stability, flight efficiency, and airport noise are considered jointly.


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    Titel :

    Aircraft design for flight below the sonic boom speed limit


    Beteiligte:
    Jones, R. T. (Autor:in)

    Erscheinungsdatum :

    1974-05-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :