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Computational Mechanics

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01.06.2015 | Original Paper

Special methods for aerodynamic-moment calculations from parachute FSI modeling

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

Erschienen in: Computational Mechanics | Ausgabe 6/2015

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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.

Vorheriger Artikel Fluid–structure interaction

Nächster Artikel Vibration of structures containing compressible liquids with surface tension and sloshing effects. Reduced-order model

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Titel: Special methods for aerodynamic-moment calculations from parachute FSI modeling
verfasst von: Kenji Takizawa
Tayfun E. Tezduyar
Cody Boswell
Yuki Tsutsui
Kenneth Montel
Publikationsdatum: 01.06.2015
Verlag: Springer Berlin Heidelberg
Erschienen in: Computational Mechanics / Ausgabe 6/2015
Print ISSN: 0178-7675
Elektronische ISSN: 1432-0924
DOI: https://doi.org/10.1007/s00466-014-1074-5

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