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Special methods for aerodynamic-moment calculations from parachute FSI modeling

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Abstract

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.

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Acknowledgments

This work was supported in part by NASA Johnson Space Center grant NNX13AD87G. It was also supported in part by the Rice–Waseda research agreement (first author).

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Authors and Affiliations

  1. Department of Modern Mechanical Engineering and Waseda Institute for Advanced Study, Waseda University, 1-6-1 Nishi-Waseda, Shinjuku-ku, Tokyo, 169-8050, Japan

    Kenji Takizawa & Yuki Tsutsui

  2. Mechanical Engineering, Rice University, MS 321, 6100 Main Street, Houston, TX, 77005, USA

    Tayfun E. Tezduyar, Cody Boswell & Kenneth Montel

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  1. Kenji Takizawa
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  2. Tayfun E. Tezduyar
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  3. Cody Boswell
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  4. Yuki Tsutsui
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  5. Kenneth Montel
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Correspondence to Tayfun E. Tezduyar.

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Takizawa, K., Tezduyar, T.E., Boswell, C. et al. Special methods for aerodynamic-moment calculations from parachute FSI modeling. Comput Mech 55, 1059–1069 (2015). https://doi.org/10.1007/s00466-014-1074-5

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