This paper documents a process for analyzing whether a particular supersonic aircraft configuration layout and a given cruise condition are feasible to achieve a trimmed low-boom design. This process was motivated by the need to know whether a particular configuration at a given cruise condition could be reshaped to satisfy both low-boom and flight trim constraints. Without such a process, much effort could be wasted on shaping a configuration layout at a cruise condition that could never satisfy both low-boom and flight trim constraints simultaneously. The process helps to exclude infeasible configuration layouts with minimum effort and allows a designer to develop trimmed low-boom concepts more effectively. A notional low-boom supersonic demonstrator concept is used to illustrate the analysis/design process.


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    Titel :

    Feasibility of Supersonic Aircraft Concepts for Low-Boom and Flight Trim Constraints


    Beteiligte:
    Li, Wu (Autor:in)

    Kongress:

    AIAA Applied Aerodynamics Conference ; 2015 ; Dallas, TX, United States


    Erscheinungsdatum :

    2015-06-22


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Conceptual Design of Low-Boom Supersonic Aircraft with Flight Trim Requirement

    Ordaz, Irian / Geiselhart, Karl / Fenbert, James W. | AIAA | 2014


    Conceptual Design of Low-Boom Aircraft with Flight Trim Requirement

    Ordaz, Irian / Geiselhart, Karl A. / Fenbert, James W. | NTRS | 2014


    Conceptual Design of Low-Boom Aircraft with Flight Trim Requirement

    Ordaz, Irian / Geiselhart, Karl A. / Fenbert, James W. | AIAA | 2015