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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    ICAS2016_0714: NUMERICAL STUDY OF ACTIVE SHOCK WAVE-TURBULENT BOUNDARY LAYER INTERACTION CONTROL FOR TRANSONIC AERODYNAMICS

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




    Numerical study of strake aerodynamics

    Kerlick, G.D. / Klopfer, G.H. / Nixon, D. | Tema Archive | 1982