A survey is presented of factors affecting blunt leading-edge separation for swept and semi-slender wings. This class of separation often results in the onset and progression of separation-induced vortical flow over a slender or semi-slender wing. The term semi-slender is used to distinguish wings with moderate sweeps and aspect ratios from the more traditional highly-swept, low-aspect-ratio slender wing. Emphasis is divided between a selection of results obtained through literature survey a section of results from some recent research projects primarily being coordinated through NATO s Research and Technology Organization (RTO). An aircraft context to these studies is included.


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    Titel :

    A Survey of Factors Affecting Blunt Leading-Edge Separation for Swept and Semi-Slender Wings


    Beteiligte:

    Kongress:

    28th AIAA Applied Aerodynamics Conference ; 2010 ; Chicago, IL, United States


    Erscheinungsdatum :

    28.06.2010


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    A Survey of Factors Affecting Blunt-Leading-Edge Separation for Swept and Semi-Slender Wings

    Luckring, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010



    On Slender Delta Wings with Leading-edge Separation

    Brown, Clinton E / Michael, William H , Jr | NTRS | 1955


    On slender delta wings with leading-edge separation

    Brown, Clinton E. / Michael, William H. | TIBKAT | 1955