Special methods for aerodynamic-moment calculations from parachute FSI modeling

Kenji Takizawa, Tayfun E. Tezduyar, Cody Boswell, Yuki Tsutsui, Kenneth Montel

    研究成果: Article

    49 引用 (Scopus)

    抜粋

    The space–time fluid–structure interaction (STFSI) methods for 3D parachute modeling are now at a level where they can bring reliable, practical analysis to some of the most complex parachute systems, such as spacecraft parachutes. The methods include the Deforming-Spatial-Domain/Stabilized ST method as the core computational technology, and a good number of special FSI methods targeting parachutes. Evaluating the stability characteristics of a parachute based on how the aerodynamic moment varies as a function of the angle of attack is one of the practical analyses that reliable parachute FSI modeling can deliver. We describe the special FSI methods we developed for this specific purpose and present the aerodynamic-moment data obtained from FSI modeling of NASA Orion spacecraft parachutes and Japan Aerospace Exploration Agency (JAXA) subscale parachutes.

    元の言語English
    ページ(範囲)1059-1069
    ページ数11
    ジャーナルComputational Mechanics
    55
    発行部数6
    DOI
    出版物ステータスPublished - 2014 10 30

    ASJC Scopus subject areas

    • Computational Theory and Mathematics
    • Mechanical Engineering
    • Ocean Engineering
    • Applied Mathematics
    • Computational Mathematics

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