Special methods for aerodynamic-moment calculations from parachute FSI modeling

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

    Research output: Contribution to journalArticlepeer-review

    54 Citations (Scopus)


    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.

    Original languageEnglish
    Pages (from-to)1059-1069
    Number of pages11
    JournalComputational Mechanics
    Issue number6
    Publication statusPublished - 2014 Oct 30


    • Aerodynamic moment
    • DSD/SST method
    • JAXA subscale parachutes
    • NASA Orion spacecraft parachutes
    • Space–time fluid–structure interaction methods
    • Special methods

    ASJC Scopus subject areas

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

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