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T-splines computational membrane–cable structural mechanics with continuity and smoothness: II. Spacecraft parachutes

Authors:

Takuya Terahara,

Kenji Takizawa,

Tayfun E. TezduyarAuthors Info & Claims

Computational Mechanics, Volume 71, Issue 4

Pages 677 - 686

https://doi.org/10.1007/s00466-022-02265-9

Published: 07 January 2023 Publication History

Abstract

In this second part of a two-part article, we present spacecraft parachute structural mechanics computations with the T-splines computational method introduced in the first part. The method and its implementation, which was also given in the first part, are for computations where structures with different parametric dimensions are connected with continuity and smoothness. The basis functions of the method were derived in the context of connecting structures with 2D and 1D parametric dimensions. In the first part, the 2D structure was referred to as “membrane” and the 1D structure as “cable.” The method and its implementation, however, are certainly applicable also to other 2D–1D cases, and the test computations presented in the first part included shell–cable structures. Similarly, the spacecraft parachute computations presented here are with both the membrane and shell models of the parachute canopy fabric. The computer model used in the computations is for a subscale, wind-tunnel version of the Disk–Gap–Band parachute. The computations demonstrate the effectiveness of the method in 2D–1D structural mechanics computation of spacecraft parachutes.

References

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Cited By

Wobbes EBazilevs YKuraishi TOtoguro YTakizawa KTezduyar T(2024)Complex-Geometry IGA Mesh Generation: application to structural vibrationsComputational Mechanics10.1007/s00466-023-02432-674:2(247-261)Online publication date: 1-Aug-2024
https://dl.acm.org/doi/10.1007/s00466-023-02432-6
Liu YTakizawa KTezduyar T(2024)High-resolution 3D computation of time-periodic long-wake flows with the Carrier-Domain Method and Space–Time Variational Multiscale method with isogeometric discretizationComputational Mechanics10.1007/s00466-023-02419-374:1(1-22)Online publication date: 1-Jul-2024
https://dl.acm.org/doi/10.1007/s00466-023-02419-3
Zhu QWang XDemartino CYan J(2023)Revealing aeroelastic effects on low-rise roof structures in turbulent winds via isogeometric fluid–structure interactionComputational Mechanics10.1007/s00466-023-02341-872:6(1175-1190)Online publication date: 1-Dec-2023
https://dl.acm.org/doi/10.1007/s00466-023-02341-8

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T-splines computational membrane–cable structural mechanics with continuity and smoothness: II. Spacecraft parachutes

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T-splines computational membrane–cable structural mechanics with continuity and smoothness: I. Method and implementation
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Information

Published In

cover image Computational Mechanics

Computational Mechanics Volume 71, Issue 4

Apr 2023

206 pages

ISSN:0178-7675

Issue’s Table of Contents

© The Author(s) 2023.

Publisher

Springer-Verlag

Berlin, Heidelberg

Publication History

Published: 07 January 2023

Accepted: 13 December 2022

Received: 20 November 2022

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Cited By

Wobbes EBazilevs YKuraishi TOtoguro YTakizawa KTezduyar T(2024)Complex-Geometry IGA Mesh Generation: application to structural vibrationsComputational Mechanics10.1007/s00466-023-02432-674:2(247-261)Online publication date: 1-Aug-2024
https://dl.acm.org/doi/10.1007/s00466-023-02432-6
Liu YTakizawa KTezduyar T(2024)High-resolution 3D computation of time-periodic long-wake flows with the Carrier-Domain Method and Space–Time Variational Multiscale method with isogeometric discretizationComputational Mechanics10.1007/s00466-023-02419-374:1(1-22)Online publication date: 1-Jul-2024
https://dl.acm.org/doi/10.1007/s00466-023-02419-3
Zhu QWang XDemartino CYan J(2023)Revealing aeroelastic effects on low-rise roof structures in turbulent winds via isogeometric fluid–structure interactionComputational Mechanics10.1007/s00466-023-02341-872:6(1175-1190)Online publication date: 1-Dec-2023
https://dl.acm.org/doi/10.1007/s00466-023-02341-8

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