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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    Title :

    Numerical Study of Boundary-Layer in Aerodynamics


    Contributors:

    Publication date :

    1997-07-21


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :



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