Hypersonic airbreathing vehicles are characterized by highly- integrated airframe and propulsion system. Computational Fluid Dynamics (CFD) tools have been used extensively in the design and analysis phrase of hypersonic vehicles. In this paper, an engineering method and a finite volume method based on the center of grid are developed tor preliminary research of interested integrative hypersonic vehicles with waverider configurations (cone-shaped or canard structure). Some longitudinal aerodynamic performance increments are obtained under conditions of shut-down engine or working engine. For the vehicle with canard structure, in order to study the lateral-directional stability characteristics, we also consider the influence of yaw angle on the flow field of fore-body.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Numerical Research of Airframe/Engine Integrative Hypersonic Vehicle


    Beteiligte:
    H. Yuanyan (Autor:in) / L. Jialing (Autor:in) / N. Hougli (Autor:in)

    Erscheinungsdatum :

    2002


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Hypersonic Air-Breathing Engine/Airframe Integration

    Gusev, V. N. | British Library Online Contents | 1994


    Studies of engine-airframe integrated hypersonic vehicles

    Saland, H. / Fox, H. / Hoydysh, W. | NTRS | 1972


    Studies of Engine-Airframe Integrated Hypersonic Vehicles

    H. Saland / H. Fox / W. Hoydysh | NTIS | 1972


    The integration of a hypersonic vehicle airframe with an airbreathing engine

    Gusev, V. / Blagoveshchenskij, N. / Zadonskij, S. | AIAA | 1993