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 winged aircraft offers many advantages when structure, stability, flight efficiency, and airport noise are considered jointly.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aircraft design for flight below the sonic boom speed limit


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

    Kongress:

    Quarter Century Symp. ; 1974 ; Toronto, Canada



    Erscheinungsdatum :

    1976-02-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :