Experimental and Computational Investigation of the Aerodynamics of a Supersonic Projectile with Streamwise Slots

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Abstract

    The paper investigates the role of streamwise slots applied to the boat-tail section of a supersonic projectile at Mach numbers from 1.36 to 1.83. The aerodynamic drag and surface pressures were measured in a supersonic indraft wind tunnel. Computations were performed at M = 1.36 and compared with the wind tunnel data.
    Original languageEnglish
    Title of host publication13th International Conference on Applied Mechanics, Cairo, Egypt
    Publication statusPublished - May 2008
    Event13th International Conference on Applied Mechanics, Cairo, Egypt -
    Duration: 1 Jan 1824 → …

    Conference

    Conference13th International Conference on Applied Mechanics, Cairo, Egypt
    Period1/01/24 → …

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