Numerical Simulation of a Supersonic Base Bleed Projectile with Improved Turbulence Modelling

P. Kaurinkoski, A. Hellsten

    Research output: Contribution to journalArticleScientificpeer-review

    14 Citations (Scopus)
    Original languageEnglish
    Pages (from-to)606-611
    JournalJournal of Spacecraft and Rockets
    Volume35
    Issue number5
    Publication statusPublished - 1998
    MoE publication typeA1 Journal article-refereed

    Keywords

    • aerodynamics
    • projectiles
    • stagnation point
    • turbulence modelling

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