From December 1991 to June 1992, applied aerodynamic research support was given to the team working on Low Sonic Boom configurations in the RAC branch at NASA Ames Research Center. This team developed two different configurations: a conventional wing-tail and a canard wing, in an effort to reduce the overpressure of shock waves and the accompanying noise which are projected to the ground from supersonic civil transport aircraft. A generic description of this sensitive technology is given.


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    Titel :

    Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport


    Beteiligte:

    Erscheinungsdatum :

    1995-02-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Oblique-wing sonic boom

    Hicks, R. M. / Mendoza, J. P. | NTRS | 1973


    Sonic boom of the oblique flying wing

    Van der Velden / A. / Kroo, I. | AIAA | 1994


    Sonic Boom of the Oblique Flying Wing

    Velden, A.Van der | Online Contents | 1994