The schematic representation of an aircraft’s geometry is an important part of modeling the flow about the aircraft and its vortex wake. The present monograph generalizes the approaches of many researchers employing the DVM. Among the types of aircraft representation developed up to now, the following three are the most popular and successful: plate-element, solid-element and hybrid representations.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The Near Vortex Wake Behind a Single Aircraft


    Additional title:

    Foundations Engineering Mechanics


    Contributors:


    Publication date :

    2009-06-13


    Size :

    5 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Far Vortex Wake Behind a Turbojet Aircraft

    Ginevsky, A.S. / Zhelannikov, A.I. | Springer Verlag | 2009


    Vortex Wake Behind a Helicopter

    A. Larin | NTIS | 1974




    Aircraft Vortex Wake Dynamics

    Gaifullin, A. M. / Soudakov, G. G. | SAE Technical Papers | 1996