The accomplishments made in the following three tasks are described: (1) The first task was to study shock-wave boundary-layer interactions with bleed - this study is relevant to boundary-layer control in external and mixed-compression inlets of supersonic aircraft; (2) The second task was to test RAAKE, a code developed for computing turbulence quantities; and (3) The third task was to compute flow around the Ames ER-2 aircraft that has been retrofitted with containers over its wings and fuselage. The appendices include two reports submitted to AIAA for publication.


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    Titel :

    Numerical Study of Boundary-Layer in Aerodynamics


    Beteiligte:
    T. I. P. Shih (Autor:in)

    Erscheinungsdatum :

    1997


    Format / Umfang :

    52 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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    Moghadam, Z. Seifollahi / Jahangirian, A. | British Library Conference Proceedings | 2016




    Development of a Rapid Inviscid/Boundary-Layer Aerodynamics Tool

    Ward, Alexander D. / Smart, Michael K. / Gollan, Rowan J. | AIAA | 2018