Development of a multipurpose test rig - TAILTEST

The paper discusses an innovative multipurpose test rig designed with the aim of full-scale rotorcraft fin verification. The developed test rig includes a load application mechanism able to distribute loads representative for rotorcraft tail structure. Both conventional metallic components and innov...

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Autores principales:	Oberthor Martin, Horák Václav, Růžek Roman
Formato:	article
Lenguaje:	EN FR
Publicado:	EDP Sciences 2021
Materias:	Engineering (General). Civil engineering (General) TA1-2040
Acceso en línea:	https://doaj.org/article/a9d838ad3f5d4e62854149f9a0c986d6
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spelling	oai:doaj.org-article:a9d838ad3f5d4e62854149f9a0c986d62021-12-02T17:13:47ZDevelopment of a multipurpose test rig - TAILTEST2261-236X10.1051/matecconf/202134904017https://doaj.org/article/a9d838ad3f5d4e62854149f9a0c986d62021-01-01T00:00:00Zhttps://www.matec-conferences.org/articles/matecconf/pdf/2021/18/matecconf_iceaf2021_04017.pdfhttps://doaj.org/toc/2261-236XThe paper discusses an innovative multipurpose test rig designed with the aim of full-scale rotorcraft fin verification. The developed test rig includes a load application mechanism able to distribute loads representative for rotorcraft tail structure. Both conventional metallic components and innovative thermoplastic composites are used in the rotorcraft tail structure. The test rig will be designed so that a variable stiffness of the fuselage to the fin joint is achieved. Verification of the new tail structure is supported by additional experiments and numerical analyses.Oberthor MartinHorák VáclavRůžek RomanEDP SciencesarticleEngineering (General). Civil engineering (General)TA1-2040ENFRMATEC Web of Conferences, Vol 349, p 04017 (2021)
institution	DOAJ
collection	DOAJ
language	EN FR
topic	Engineering (General). Civil engineering (General) TA1-2040
spellingShingle	Engineering (General). Civil engineering (General) TA1-2040 Oberthor Martin Horák Václav Růžek Roman Development of a multipurpose test rig - TAILTEST
description	The paper discusses an innovative multipurpose test rig designed with the aim of full-scale rotorcraft fin verification. The developed test rig includes a load application mechanism able to distribute loads representative for rotorcraft tail structure. Both conventional metallic components and innovative thermoplastic composites are used in the rotorcraft tail structure. The test rig will be designed so that a variable stiffness of the fuselage to the fin joint is achieved. Verification of the new tail structure is supported by additional experiments and numerical analyses.
format	article
author	Oberthor Martin Horák Václav Růžek Roman
author_facet	Oberthor Martin Horák Václav Růžek Roman
author_sort	Oberthor Martin
title	Development of a multipurpose test rig - TAILTEST
title_short	Development of a multipurpose test rig - TAILTEST
title_full	Development of a multipurpose test rig - TAILTEST
title_fullStr	Development of a multipurpose test rig - TAILTEST
title_full_unstemmed	Development of a multipurpose test rig - TAILTEST
title_sort	development of a multipurpose test rig - tailtest
publisher	EDP Sciences
publishDate	2021
url	https://doaj.org/article/a9d838ad3f5d4e62854149f9a0c986d6
work_keys_str_mv	AT oberthormartin developmentofamultipurposetestrigtailtest AT horakvaclav developmentofamultipurposetestrigtailtest AT ruzekroman developmentofamultipurposetestrigtailtest
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Development of a multipurpose test rig - TAILTEST

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