A multi-body aerospace apparatus includes a first aerospace body (12), a second aerospace body (14), and a flow separation member (18). The second aerospace body is attached adjacent to the first aerospace body with a gap (20) disposed between the first aerospace body and the second aerospace body. The flow separation member is attached to the first aerospace body or to the second aerospace body.


    Access

    Download


    Export, share and cite



    Title :

    Unsteady aerodynamics mitigation for multi-body aerospace apparatus


    Additional title:

    Minderung instationärer Aerodynamik für Mehrkörper-Raumfahrvorrichtung
    Atténuation d'aérodynamisme non stationnaire pour appareil aérospatial multicorps


    Contributors:

    Publication date :

    2020-09-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64G Raumfahrt , COSMONAUTICS



    Unsteady Aerodynamics of a Rapidly Tumbling Bluff Body

    Chintalapati, S. / Rock, S. G. / Habchi, S. D. et al. | British Library Conference Proceedings | 1999


    Unsteady transonic aerodynamics

    American Institute of Aeronautics and Astronautics | TIBKAT | 1989


    Unsteady aerodynamics testing

    Online Contents | 1993


    Unsteady aerodynamics

    Platzer, M. F. | NTRS | 1967


    Unsteady Aerodynamics of Vehicles

    ANDREW G. HAMMIT | AIAA | 1975