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

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dc.citation.firstpage677en_US
dc.citation.journalTitleComputational Mechanicsen_US
dc.citation.lastpage686en_US
dc.citation.volumeNumber71en_US
dc.contributor.authorTerahara, Takuyaen_US
dc.contributor.authorTakizawa, Kenjien_US
dc.contributor.authorAvsar, Rehaen_US
dc.contributor.authorTezduyar, Tayfun E.en_US
dc.date.accessioned2023-03-10T19:04:18Zen_US
dc.date.available2023-03-10T19:04:18Zen_US
dc.date.issued2023en_US
dc.description.abstractIn 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.en_US
dc.identifier.citationTerahara, Takuya, Takizawa, Kenji, Avsar, Reha, et al.. "T-splines computational membrane–cable structural mechanics with continuity and smoothness: II. Spacecraft parachutes." <i>Computational Mechanics,</i> 71, (2023) Springer Nature: 677-686. https://doi.org/10.1007/s00466-022-02265-9.en_US
dc.identifier.digitals00466-022-02265-9en_US
dc.identifier.doihttps://doi.org/10.1007/s00466-022-02265-9en_US
dc.identifier.urihttps://hdl.handle.net/1911/114510en_US
dc.language.isoengen_US
dc.publisherSpringer Natureen_US
dc.rightsThis article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons licence, and indicate if changes were made. The images or other third party material in this article are included in the article’s Creative Commons licence, unless indicated otherwise in a credit line to the material. If material is not included in the article’s Creative Commons licence and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this licence, visit http://creativecommons.org/licenses/by/4.0/.en_US
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/.en_US
dc.titleT-splines computational membrane–cable structural mechanics with continuity and smoothness: II. Spacecraft parachutesen_US
dc.typeJournal articleen_US
dc.type.dcmiTexten_US
dc.type.publicationpublisher versionen_US
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