A number of optimization problems are posed and solved for supersonic aircraft flight subject to the condition that a shock wave appears only incipiently in the sonic boom signal at a given point. The principal result is one giving the maximum effective gross weight of an aircraft of given effective length under given flight conditions. The calculus of variations with inequality constraints is used, with the novel features of a non-local isoperimetric relation and of only an upper bound on a control variable.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Optimum configurations for bangless sonic booms.


    Beteiligte:


    Erscheinungsdatum :

    01.10.1972


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Sonic Booms in Atmospheric Turbulence (SonicBAT): The Influence of Turbulence on Shaped Sonic Booms

    Bradley, Kevin A. / Hobbs, Christopher M. / Wilmer, Clifton B. et al. | NTRS | 2020


    Seismic effects of sonic booms

    Goforth, Tom T. / MacDonald, John A. | TIBKAT | 1968


    Supersonic transport secondary sonic booms

    Poling, Hugh / Robinson, L. / Sutherland, Louis | AIAA | 1997