SYSTEM AND METHOD FOR MINIMIZING WAVE DRAG THROUGH BILATERALLY ASYMMETRIC DESIGN An air vehicle (100) having a bilaterally asymmetric configuration may include a body (104) having a longitudinal axis (106). The air vehicle (100) may further include longitudinally offset engine nacelles (232), asymmetrically lengthened engine nacelles (232), and/or longitudinally offset protruding aerodynamic surfaces (190). 04 CN Co CN CN C\I 'C 0 00c CD Co C,4 CN 0 CN r- C%4C) CNC0 C*4 o 00


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    System and method for minimizing wave drag through bilaterally asymmetric design


    Beteiligte:
    PFLUG WILLIAM (Autor:in) / TILLOTSON BRIAN J (Autor:in)

    Erscheinungsdatum :

    16.02.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    BILATERALLY ASYMMETRIC DESIGN FOR MINIMIZING WAVE DRAG

    PFLUG WILLIAM / TILLOTSON BRIAN J | Europäisches Patentamt | 2015

    Freier Zugriff

    Bilaterally asymmetric design for minimizing wave drag

    PFLUG WILLIAM / TILLOTSON BRIAN J | Europäisches Patentamt | 2016

    Freier Zugriff

    System and method for minimizing wave drag through bilaterally asymmetric design

    PFLUG WILLIAM / TILLOTSON BRIAN J | Europäisches Patentamt | 2017

    Freier Zugriff

    SYSTEM AND METHOD FOR MINIMIZING WAVE DRAG THROUGH BILATERALLY ASYMMETRIC DESIGN

    PFLUG WILLIAM / TILLOTSON BRIAN J | Europäisches Patentamt | 2016

    Freier Zugriff

    Parameter design method of bilaterally LCC compensated BIPT system

    WU XIAORUI / CHEN SHAONAN / HOU JIAHE et al. | Europäisches Patentamt | 2024

    Freier Zugriff