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Compressible vortex loops in a shock tube with helium driver

  • Raffaello Mariani
  • , Konstantinos Kontis

    Research output: Chapter in Book/Conference proceedingConference contributionpeer-review

    Abstract

    An experimental study has been conducted on the generation and propagation of compressible vortex loops using helium as a driver gas. The study aimed at evaluating the flow characteristics of a compressible vortex loop generated using a lighter then air gas into air at ambient conditions. The advantage of such system when compared to a constant gas system based on ambient air is to effectively increase the Mach number while keeping the pressure ratio constant. Three driver pressures were used (4, 8, and 12bar) generating a theoretical Mach number value of 1.53, 1.89, and 2.12 respectively. Qualitative and quantitatve analysis were conducted. The generation of secondary vortex rings ahead of the main vortex ring were witnessed at all driver pressure. The structure of the trailing jet behind the vortex ring is shown to transition from a regular to a Mach reflection with increasing Mach disk size. The presence of the Mach disk results in the generation of vortical flow inside the main trailing jet with opposite circulation with respect to the outer jet boundary. Copyright © 2011 by Raffaello Mariani.
    Original languageEnglish
    Title of host publication49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition|AIAA Aerosp. Sci. Meet. Incl. New Horiz. Forum Aerosp. Expos.
    Subtitle of host publicationAIAA-2011-989
    PublisherAmerican Institute of Aeronautics and Astronautics
    Publication statusPublished - 2011
    Event49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Orlando, FL
    Duration: 1 Jul 2011 → …

    Conference

    Conference49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
    CityOrlando, FL
    Period1/07/11 → …

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