• Català
  • Castellano
  • English
Logo Catalònica
  • Cerca
  • Col·leccions
  • Coneix-nos
  • Ajuda
  • Directori
  • Professionals
Està a:  › Dades de registre
Linked Open Data
2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench
Identificadors del recurs
http://hdl.handle.net/10256/23111
Procedència
(DUGiDocs. Recerca)

Fitxa

Títol:
2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench
Matèria:
Assaigs de materials -- Congressos
Materials -- Testing -- Congresses
Indústria aeronàutica -- Congressos
Aircraft industry -- Congresses
Descripció:
The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample
Font:
CompTest 2023
Idioma:
English
Autor/Productor:
Castanié, Bruno
Passieux, Jean-Charles
Périé, Jean-Noel
Bouvet, Christophe
Serra, Joël
Editor:
Universitat de Girona. Grup de Recerca en Anàlisi i Materials Avançats per al Disseny Estructural (AMADE)
Drets:
Tots els drets reservats
info:eu-repo/semantics/openAccess
Data:
2023-05-31
Tipus de recurs:
slide
Format:
application/pdf

oai_dc

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < oai_dc:dc schemaLocation =" http://www.openarchives.org/OAI/2.0/oai_dc/ http://www.openarchives.org/OAI/2.0/oai_dc.xsd " >

    1. < dc:title > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ dc:title >

    2. < dc:creator > Castanié, Bruno </ dc:creator >

    3. < dc:creator > Passieux, Jean-Charles </ dc:creator >

    4. < dc:creator > Périé, Jean-Noel </ dc:creator >

    5. < dc:creator > Bouvet, Christophe </ dc:creator >

    6. < dc:creator > Serra, Joël </ dc:creator >

    7. < dc:subject > Assaigs de materials -- Congressos </ dc:subject >

    8. < dc:subject > Materials -- Testing -- Congresses </ dc:subject >

    9. < dc:subject > Indústria aeronàutica -- Congressos </ dc:subject >

    10. < dc:subject > Aircraft industry -- Congresses </ dc:subject >

    11. < dc:description > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ dc:description >

    12. < dc:date > 2023-05-31 </ dc:date >

    13. < dc:type > slide </ dc:type >

    14. < dc:identifier > http://hdl.handle.net/10256/23111 </ dc:identifier >

    15. < dc:language > eng </ dc:language >

    16. < dc:source > CompTest 2023 </ dc:source >

    17. < dc:rights > Tots els drets reservats </ dc:rights >

    18. < dc:rights > info:eu-repo/semantics/openAccess </ dc:rights >

    19. < dc:format > application/pdf </ dc:format >

    20. < dc:publisher > Universitat de Girona. Grup de Recerca en Anàlisi i Materials Avançats per al Disseny Estructural (AMADE) </ dc:publisher >

    </ oai_dc:dc >

didl

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < d:DIDL schemaLocation =" urn:mpeg:mpeg21:2002:02-DIDL-NS http://standards.iso.org/ittf/PubliclyAvailableStandards/MPEG-21_schema_files/did/didl.xsd " >

    1. < d:DIDLInfo >

      1. < dcterms:created schemaLocation =" http://purl.org/dc/terms/ http://dublincore.org/schemas/xmls/qdc/dcterms.xsd " > 2023-06-23T11:15:45Z </ dcterms:created >

      </ d:DIDLInfo >

    2. < d:Item id =" hdl_10256_23111 " >

      1. < d:Descriptor >

        1. < d:Statement mimeType =" application/xml; charset=utf-8 " >

          1. < dii:Identifier schemaLocation =" urn:mpeg:mpeg21:2002:01-DII-NS http://standards.iso.org/ittf/PubliclyAvailableStandards/MPEG-21_schema_files/dii/dii.xsd " > urn:hdl:10256/23111 </ dii:Identifier >

          </ d:Statement >

        </ d:Descriptor >

      2. < d:Descriptor >

        1. < d:Statement mimeType =" application/xml; charset=utf-8 " >

          1. < oai_dc:dc schemaLocation =" http://www.openarchives.org/OAI/2.0/oai_dc/ http://www.openarchives.org/OAI/2.0/oai_dc.xsd " >

            1. < dc:title > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ dc:title >

            2. < dc:creator > Castanié, Bruno </ dc:creator >

            3. < dc:creator > Passieux, Jean-Charles </ dc:creator >

            4. < dc:creator > Périé, Jean-Noel </ dc:creator >

            5. < dc:creator > Bouvet, Christophe </ dc:creator >

            6. < dc:creator > Serra, Joël </ dc:creator >

            7. < dc:subject > Assaigs de materials -- Congressos </ dc:subject >

            8. < dc:subject > Materials -- Testing -- Congresses </ dc:subject >

            9. < dc:subject > Indústria aeronàutica -- Congressos </ dc:subject >

            10. < dc:subject > Aircraft industry -- Congresses </ dc:subject >

            11. < dc:description > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ dc:description >

            12. < dc:date > 2023-06-23T11:15:45Z </ dc:date >

            13. < dc:date > 2023-06-23T11:15:45Z </ dc:date >

            14. < dc:date > 2023-05-31 </ dc:date >

            15. < dc:type > slide </ dc:type >

            16. < dc:identifier > http://hdl.handle.net/10256/23111 </ dc:identifier >

            17. < dc:language > eng </ dc:language >

            18. < dc:relation > CompTest 2023 </ dc:relation >

            19. < dc:rights > info:eu-repo/semantics/openAccess </ dc:rights >

            20. < dc:rights > Tots els drets reservats </ dc:rights >

            21. < dc:publisher > Universitat de Girona. Grup de Recerca en Anàlisi i Materials Avançats per al Disseny Estructural (AMADE) </ dc:publisher >

            </ oai_dc:dc >

          </ d:Statement >

        </ d:Descriptor >

      3. < d:Component id =" 10256_23111_1 " >

        1. < d:Resource mimeType =" application/pdf " ref =" https://dugi-doc.udg.edu/bitstream/10256/23111/1/02-11-Or-R033-20230531.pdf " />

        </ d:Component >

      4. < d:Component id =" 10256_23111_2 " >

        1. < d:Resource mimeType =" application/pdf " ref =" https://dugi-doc.udg.edu/bitstream/10256/23111/2/R033+-+Castani%C3%A9.pdf " />

        </ d:Component >

      </ d:Item >

    </ d:DIDL >

dim

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < dim:dim schemaLocation =" http://www.dspace.org/xmlns/dspace/dim http://www.dspace.org/schema/dim.xsd " >

    1. < dim:field element =" contributor " mdschema =" dc " qualifier =" author " > Castanié, Bruno </ dim:field >

    2. < dim:field element =" contributor " mdschema =" dc " qualifier =" author " > Passieux, Jean-Charles </ dim:field >

    3. < dim:field element =" contributor " mdschema =" dc " qualifier =" author " > Périé, Jean-Noel </ dim:field >

    4. < dim:field element =" contributor " mdschema =" dc " qualifier =" author " > Bouvet, Christophe </ dim:field >

    5. < dim:field element =" contributor " mdschema =" dc " qualifier =" author " > Serra, Joël </ dim:field >

    6. < dim:field element =" date " mdschema =" dc " qualifier =" accessioned " > 2023-06-23T11:15:45Z </ dim:field >

    7. < dim:field element =" date " mdschema =" dc " qualifier =" available " > 2023-06-23T11:15:45Z </ dim:field >

    8. < dim:field element =" date " mdschema =" dc " qualifier =" issued " > 2023-05-31 </ dim:field >

    9. < dim:field element =" identifier " mdschema =" dc " qualifier =" uri " > http://hdl.handle.net/10256/23111 </ dim:field >

    10. < dim:field element =" description " lang =" cat " mdschema =" dc " qualifier =" abstract " > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ dim:field >

    11. < dim:field element =" description " lang =" en " mdschema =" dc " qualifier =" provenance " > Submitted by Claudia Plana (claudia.plana@udg.edu) on 2023-06-23T11:15:45Z No. of bitstreams: 2 02-11-Or-R033-20230531.pdf: 1726762 bytes, checksum: be15ffd16c35c24bf2b320d5e7e7274c (MD5) R033 - Castanié.pdf: 224481 bytes, checksum: be57f431673711d034109a723435cc3e (MD5) </ dim:field >

    12. < dim:field element =" description " lang =" en " mdschema =" dc " qualifier =" provenance " > Made available in DSpace on 2023-06-23T11:15:45Z (GMT). No. of bitstreams: 2 02-11-Or-R033-20230531.pdf: 1726762 bytes, checksum: be15ffd16c35c24bf2b320d5e7e7274c (MD5) R033 - Castanié.pdf: 224481 bytes, checksum: be57f431673711d034109a723435cc3e (MD5) Previous issue date: 2023-05-31 </ dim:field >

    13. < dim:field element =" format " lang =" cat " mdschema =" dc " qualifier =" mimetype " > application/pdf </ dim:field >

    14. < dim:field element =" language " lang =" cat " mdschema =" dc " qualifier =" iso " > eng </ dim:field >

    15. < dim:field element =" publisher " lang =" cat " mdschema =" dc " > Universitat de Girona. Grup de Recerca en Anàlisi i Materials Avançats per al Disseny Estructural (AMADE) </ dim:field >

    16. < dim:field element =" relation " lang =" cat " mdschema =" dc " qualifier =" ispartofseries " > CompTest 2023 </ dim:field >

    17. < dim:field element =" rights " mdschema =" dc " > Tots els drets reservats </ dim:field >

    18. < dim:field element =" rights " lang =" cat " mdschema =" dc " qualifier =" accessRights " > info:eu-repo/semantics/openAccess </ dim:field >

    19. < dim:field element =" subject " lang =" cat " mdschema =" dc " > Assaigs de materials -- Congressos </ dim:field >

    20. < dim:field element =" subject " lang =" cat " mdschema =" dc " > Materials -- Testing -- Congresses </ dim:field >

    21. < dim:field element =" subject " lang =" cat " mdschema =" dc " > Indústria aeronàutica -- Congressos </ dim:field >

    22. < dim:field element =" subject " lang =" cat " mdschema =" dc " > Aircraft industry -- Congresses </ dim:field >

    23. < dim:field element =" title " lang =" cat " mdschema =" dc " > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ dim:field >

    24. < dim:field element =" type " lang =" cat " mdschema =" dc " > slide </ dim:field >

    </ dim:dim >

edm

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < rdf:RDF schemaLocation =" http://www.w3.org/1999/02/22-rdf-syntax-ns# http://www.europeana.eu/schemas/edm/EDM.xsd " >

    1. < edm:ProvidedCHO about =" https://catalonica.bnc.cat/catalonicahub/lod/oai:dugi-doc.udg.edu:10256_--_23111#ent0 " >

      1. < dc:creator > Castanié, Bruno </ dc:creator >

      2. < dc:creator > Passieux, Jean-Charles </ dc:creator >

      3. < dc:creator > Périé, Jean-Noel </ dc:creator >

      4. < dc:creator > Bouvet, Christophe </ dc:creator >

      5. < dc:creator > Serra, Joël </ dc:creator >

      6. < dc:date > 2023-05-31 </ dc:date >

      7. < dc:description > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ dc:description >

      8. < dc:identifier > http://hdl.handle.net/10256/23111 </ dc:identifier >

      9. < dc:language > eng </ dc:language >

      10. < dc:publisher > Universitat de Girona. Grup de Recerca en Anàlisi i Materials Avançats per al Disseny Estructural (AMADE) </ dc:publisher >

      11. < dc:rights > Tots els drets reservats </ dc:rights >

      12. < dc:rights > info:eu-repo/semantics/openAccess </ dc:rights >

      13. < dc:source > CompTest 2023 </ dc:source >

      14. < dc:subject > Assaigs de materials -- Congressos </ dc:subject >

      15. < dc:subject > Materials -- Testing -- Congresses </ dc:subject >

      16. < dc:subject > Indústria aeronàutica -- Congressos </ dc:subject >

      17. < dc:subject > Aircraft industry -- Congresses </ dc:subject >

      18. < dc:title > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ dc:title >

      19. < dc:type > slide </ dc:type >

      20. < edm:type > TEXT </ edm:type >

      </ edm:ProvidedCHO >

    2. < ore:Aggregation about =" https://catalonica.bnc.cat/catalonicahub/lod/oai:dugi-doc.udg.edu:10256_--_23111#ent1 " >

      1. < edm:aggregatedCHO resource =" https://catalonica.bnc.cat/catalonicahub/lod/oai:dugi-doc.udg.edu:10256_--_23111#ent0 " />
      2. < edm:dataProvider > DUGiDocs. Recerca </ edm:dataProvider >

      3. < edm:isShownAt resource =" http://hdl.handle.net/10256/23111 " />
      4. < edm:isShownBy resource =" https://dugi-doc.udg.edu/bitstream/10256/23111/1/02-11-Or-R033-20230531.pdf " />
      5. < edm:provider > Catalònica </ edm:provider >

      6. < edm:rights resource =" http://creativecommons.org/licenses/by-nc-nd/4.0/ " />

      </ ore:Aggregation >

    </ rdf:RDF >

etdms

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < thesis schemaLocation =" http://www.ndltd.org/standards/metadata/etdms/1.0/ http://www.ndltd.org/standards/metadata/etdms/1.0/etdms.xsd " >

    1. < title > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ title >

    2. < creator > Castanié, Bruno </ creator >

    3. < creator > Passieux, Jean-Charles </ creator >

    4. < creator > Périé, Jean-Noel </ creator >

    5. < creator > Bouvet, Christophe </ creator >

    6. < creator > Serra, Joël </ creator >

    7. < subject > Assaigs de materials -- Congressos </ subject >

    8. < subject > Materials -- Testing -- Congresses </ subject >

    9. < subject > Indústria aeronàutica -- Congressos </ subject >

    10. < subject > Aircraft industry -- Congresses </ subject >

    11. < description > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ description >

    12. < date > 2023-06-23 </ date >

    13. < date > 2023-06-23 </ date >

    14. < date > 2023-05-31 </ date >

    15. < type > slide </ type >

    16. < identifier > http://hdl.handle.net/10256/23111 </ identifier >

    17. < language > eng </ language >

    18. < relation > CompTest 2023 </ relation >

    19. < rights > info:eu-repo/semantics/openAccess </ rights >

    20. < rights > Tots els drets reservats </ rights >

    21. < publisher > Universitat de Girona. Grup de Recerca en Anàlisi i Materials Avançats per al Disseny Estructural (AMADE) </ publisher >

    </ thesis >

marc

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < record schemaLocation =" http://www.loc.gov/MARC21/slim http://www.loc.gov/standards/marcxml/schema/MARC21slim.xsd " >

    1. < leader > 00925njm 22002777a 4500 </ leader >

    2. < datafield ind1 =" " ind2 =" " tag =" 042 " >

      1. < subfield code =" a " > dc </ subfield >

      </ datafield >

    3. < datafield ind1 =" " ind2 =" " tag =" 720 " >

      1. < subfield code =" a " > Castanié, Bruno </ subfield >

      2. < subfield code =" e " > author </ subfield >

      </ datafield >

    4. < datafield ind1 =" " ind2 =" " tag =" 720 " >

      1. < subfield code =" a " > Passieux, Jean-Charles </ subfield >

      2. < subfield code =" e " > author </ subfield >

      </ datafield >

    5. < datafield ind1 =" " ind2 =" " tag =" 720 " >

      1. < subfield code =" a " > Périé, Jean-Noel </ subfield >

      2. < subfield code =" e " > author </ subfield >

      </ datafield >

    6. < datafield ind1 =" " ind2 =" " tag =" 720 " >

      1. < subfield code =" a " > Bouvet, Christophe </ subfield >

      2. < subfield code =" e " > author </ subfield >

      </ datafield >

    7. < datafield ind1 =" " ind2 =" " tag =" 720 " >

      1. < subfield code =" a " > Serra, Joël </ subfield >

      2. < subfield code =" e " > author </ subfield >

      </ datafield >

    8. < datafield ind1 =" " ind2 =" " tag =" 260 " >

      1. < subfield code =" c " > 2023-05-31 </ subfield >

      </ datafield >

    9. < datafield ind1 =" " ind2 =" " tag =" 520 " >

      1. < subfield code =" a " > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ subfield >

      </ datafield >

    10. < datafield ind1 =" 8 " ind2 =" " tag =" 024 " >

      1. < subfield code =" a " > http://hdl.handle.net/10256/23111 </ subfield >

      </ datafield >

    11. < datafield ind1 =" " ind2 =" " tag =" 653 " >

      1. < subfield code =" a " > Assaigs de materials -- Congressos </ subfield >

      </ datafield >

    12. < datafield ind1 =" " ind2 =" " tag =" 653 " >

      1. < subfield code =" a " > Materials -- Testing -- Congresses </ subfield >

      </ datafield >

    13. < datafield ind1 =" " ind2 =" " tag =" 653 " >

      1. < subfield code =" a " > Indústria aeronàutica -- Congressos </ subfield >

      </ datafield >

    14. < datafield ind1 =" " ind2 =" " tag =" 653 " >

      1. < subfield code =" a " > Aircraft industry -- Congresses </ subfield >

      </ datafield >

    15. < datafield ind1 =" 0 " ind2 =" 0 " tag =" 245 " >

      1. < subfield code =" a " > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ subfield >

      </ datafield >

    </ record >

mets

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < mets ID =" DSpace_ITEM_10256-23111 " OBJID =" hdl:10256/23111 " PROFILE =" DSpace METS SIP Profile 1.0 " TYPE =" DSpace ITEM " schemaLocation =" http://www.loc.gov/METS/ http://www.loc.gov/standards/mets/mets.xsd " >

    1. < metsHdr CREATEDATE =" 2023-10-04T23:13:14Z " >

      1. < agent ROLE =" CUSTODIAN " TYPE =" ORGANIZATION " >

        1. < name > DUGiDocs </ name >

        </ agent >

      </ metsHdr >

    2. < dmdSec ID =" DMD_10256_23111 " >

      1. < mdWrap MDTYPE =" MODS " >

        1. < xmlData schemaLocation =" http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-1.xsd " >

          1. < mods:mods schemaLocation =" http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-1.xsd " >

            1. < mods:name >

              1. < mods:role >

                1. < mods:roleTerm type =" text " > author </ mods:roleTerm >

                </ mods:role >

              2. < mods:namePart > Castanié, Bruno </ mods:namePart >

              </ mods:name >

            2. < mods:name >

              1. < mods:role >

                1. < mods:roleTerm type =" text " > author </ mods:roleTerm >

                </ mods:role >

              2. < mods:namePart > Passieux, Jean-Charles </ mods:namePart >

              </ mods:name >

            3. < mods:name >

              1. < mods:role >

                1. < mods:roleTerm type =" text " > author </ mods:roleTerm >

                </ mods:role >

              2. < mods:namePart > Périé, Jean-Noel </ mods:namePart >

              </ mods:name >

            4. < mods:name >

              1. < mods:role >

                1. < mods:roleTerm type =" text " > author </ mods:roleTerm >

                </ mods:role >

              2. < mods:namePart > Bouvet, Christophe </ mods:namePart >

              </ mods:name >

            5. < mods:name >

              1. < mods:role >

                1. < mods:roleTerm type =" text " > author </ mods:roleTerm >

                </ mods:role >

              2. < mods:namePart > Serra, Joël </ mods:namePart >

              </ mods:name >

            6. < mods:extension >

              1. < mods:dateAccessioned encoding =" iso8601 " > 2023-06-23T11:15:45Z </ mods:dateAccessioned >

              </ mods:extension >

            7. < mods:extension >

              1. < mods:dateAvailable encoding =" iso8601 " > 2023-06-23T11:15:45Z </ mods:dateAvailable >

              </ mods:extension >

            8. < mods:originInfo >

              1. < mods:dateIssued encoding =" iso8601 " > 2023-05-31 </ mods:dateIssued >

              </ mods:originInfo >

            9. < mods:identifier type =" uri " > http://hdl.handle.net/10256/23111 </ mods:identifier >

            10. < mods:abstract > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ mods:abstract >

            11. < mods:language >

              1. < mods:languageTerm authority =" rfc3066 " > eng </ mods:languageTerm >

              </ mods:language >

            12. < mods:accessCondition type =" useAndReproduction " > Tots els drets reservats </ mods:accessCondition >

            13. < mods:subject >

              1. < mods:topic > Assaigs de materials -- Congressos </ mods:topic >

              </ mods:subject >

            14. < mods:subject >

              1. < mods:topic > Materials -- Testing -- Congresses </ mods:topic >

              </ mods:subject >

            15. < mods:subject >

              1. < mods:topic > Indústria aeronàutica -- Congressos </ mods:topic >

              </ mods:subject >

            16. < mods:subject >

              1. < mods:topic > Aircraft industry -- Congresses </ mods:topic >

              </ mods:subject >

            17. < mods:titleInfo >

              1. < mods:title > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ mods:title >

              </ mods:titleInfo >

            18. < mods:genre > slide </ mods:genre >

            </ mods:mods >

          </ xmlData >

        </ mdWrap >

      </ dmdSec >

    3. < amdSec ID =" TMD_10256_23111 " >

      1. < rightsMD ID =" RIG_10256_23111 " >

        1. < mdWrap MDTYPE =" OTHER " MIMETYPE =" text/plain " OTHERMDTYPE =" DSpaceDepositLicense " >

          1. < binData > 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 </ binData >

          </ mdWrap >

        </ rightsMD >

      </ amdSec >

    4. < amdSec ID =" FO_10256_23111_1 " >

      1. < techMD ID =" TECH_O_10256_23111_1 " >

        1. < mdWrap MDTYPE =" PREMIS " >

          1. < xmlData schemaLocation =" http://www.loc.gov/standards/premis http://www.loc.gov/standards/premis/PREMIS-v1-0.xsd " >

            1. < premis:premis >

              1. < premis:object >

                1. < premis:objectIdentifier >

                  1. < premis:objectIdentifierType > URL </ premis:objectIdentifierType >

                  2. < premis:objectIdentifierValue > https://dugi-doc.udg.edu/bitstream/10256/23111/1/02-11-Or-R033-20230531.pdf </ premis:objectIdentifierValue >

                  </ premis:objectIdentifier >

                2. < premis:objectCategory > File </ premis:objectCategory >

                3. < premis:objectCharacteristics >

                  1. < premis:fixity >

                    1. < premis:messageDigestAlgorithm > MD5 </ premis:messageDigestAlgorithm >

                    2. < premis:messageDigest > be15ffd16c35c24bf2b320d5e7e7274c </ premis:messageDigest >

                    </ premis:fixity >

                  2. < premis:size > 1726762 </ premis:size >

                  3. < premis:format >

                    1. < premis:formatDesignation >

                      1. < premis:formatName > application/pdf </ premis:formatName >

                      </ premis:formatDesignation >

                    </ premis:format >

                  </ premis:objectCharacteristics >

                4. < premis:originalName > 02-11-Or-R033-20230531.pdf </ premis:originalName >

                </ premis:object >

              </ premis:premis >

            </ xmlData >

          </ mdWrap >

        </ techMD >

      </ amdSec >

    5. < amdSec ID =" FO_10256_23111_2 " >

      1. < techMD ID =" TECH_O_10256_23111_2 " >

        1. < mdWrap MDTYPE =" PREMIS " >

          1. < xmlData schemaLocation =" http://www.loc.gov/standards/premis http://www.loc.gov/standards/premis/PREMIS-v1-0.xsd " >

            1. < premis:premis >

              1. < premis:object >

                1. < premis:objectIdentifier >

                  1. < premis:objectIdentifierType > URL </ premis:objectIdentifierType >

                  2. < premis:objectIdentifierValue > https://dugi-doc.udg.edu/bitstream/10256/23111/2/R033+-+Castani%C3%A9.pdf </ premis:objectIdentifierValue >

                  </ premis:objectIdentifier >

                2. < premis:objectCategory > File </ premis:objectCategory >

                3. < premis:objectCharacteristics >

                  1. < premis:fixity >

                    1. < premis:messageDigestAlgorithm > MD5 </ premis:messageDigestAlgorithm >

                    2. < premis:messageDigest > be57f431673711d034109a723435cc3e </ premis:messageDigest >

                    </ premis:fixity >

                  2. < premis:size > 224481 </ premis:size >

                  3. < premis:format >

                    1. < premis:formatDesignation >

                      1. < premis:formatName > application/pdf </ premis:formatName >

                      </ premis:formatDesignation >

                    </ premis:format >

                  </ premis:objectCharacteristics >

                4. < premis:originalName > R033 - Castanié.pdf </ premis:originalName >

                </ premis:object >

              </ premis:premis >

            </ xmlData >

          </ mdWrap >

        </ techMD >

      </ amdSec >

    6. < fileSec >

      1. < fileGrp USE =" ORIGINAL " >

        1. < file ADMID =" FO_10256_23111_1 " CHECKSUM =" be15ffd16c35c24bf2b320d5e7e7274c " CHECKSUMTYPE =" MD5 " GROUPID =" GROUP_BITSTREAM_10256_23111_1 " ID =" BITSTREAM_ORIGINAL_10256_23111_1 " MIMETYPE =" application/pdf " SEQ =" 1 " SIZE =" 1726762 " >

          1. < FLocat LOCTYPE =" URL " href =" https://dugi-doc.udg.edu/bitstream/10256/23111/1/02-11-Or-R033-20230531.pdf " type =" simple " />

          </ file >

        2. < file ADMID =" FO_10256_23111_2 " CHECKSUM =" be57f431673711d034109a723435cc3e " CHECKSUMTYPE =" MD5 " GROUPID =" GROUP_BITSTREAM_10256_23111_2 " ID =" BITSTREAM_ORIGINAL_10256_23111_2 " MIMETYPE =" application/pdf " SEQ =" 2 " SIZE =" 224481 " >

          1. < FLocat LOCTYPE =" URL " href =" https://dugi-doc.udg.edu/bitstream/10256/23111/2/R033+-+Castani%C3%A9.pdf " type =" simple " />

          </ file >

        </ fileGrp >

      </ fileSec >

    7. < structMap LABEL =" DSpace Object " TYPE =" LOGICAL " >

      1. < div ADMID =" DMD_10256_23111 " TYPE =" DSpace Object Contents " >

        1. < div TYPE =" DSpace BITSTREAM " >

          1. < fptr FILEID =" BITSTREAM_ORIGINAL_10256_23111_1 " />

          </ div >

        2. < div TYPE =" DSpace BITSTREAM " >

          1. < fptr FILEID =" BITSTREAM_ORIGINAL_10256_23111_2 " />

          </ div >

        </ div >

      </ structMap >

    </ mets >

mods

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < mods:mods schemaLocation =" http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-1.xsd " >

    1. < mods:name >

      1. < mods:namePart > Castanié, Bruno </ mods:namePart >

      </ mods:name >

    2. < mods:name >

      1. < mods:namePart > Passieux, Jean-Charles </ mods:namePart >

      </ mods:name >

    3. < mods:name >

      1. < mods:namePart > Périé, Jean-Noel </ mods:namePart >

      </ mods:name >

    4. < mods:name >

      1. < mods:namePart > Bouvet, Christophe </ mods:namePart >

      </ mods:name >

    5. < mods:name >

      1. < mods:namePart > Serra, Joël </ mods:namePart >

      </ mods:name >

    6. < mods:extension >

      1. < mods:dateAvailable encoding =" iso8601 " > 2023-06-23T11:15:45Z </ mods:dateAvailable >

      </ mods:extension >

    7. < mods:extension >

      1. < mods:dateAccessioned encoding =" iso8601 " > 2023-06-23T11:15:45Z </ mods:dateAccessioned >

      </ mods:extension >

    8. < mods:originInfo >

      1. < mods:dateIssued encoding =" iso8601 " > 2023-05-31 </ mods:dateIssued >

      </ mods:originInfo >

    9. < mods:identifier type =" uri " > http://hdl.handle.net/10256/23111 </ mods:identifier >

    10. < mods:abstract > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ mods:abstract >

    11. < mods:language >

      1. < mods:languageTerm > eng </ mods:languageTerm >

      </ mods:language >

    12. < mods:accessCondition type =" useAndReproduction " > info:eu-repo/semantics/openAccess </ mods:accessCondition >

    13. < mods:accessCondition type =" useAndReproduction " > Tots els drets reservats </ mods:accessCondition >

    14. < mods:subject >

      1. < mods:topic > Assaigs de materials -- Congressos </ mods:topic >

      </ mods:subject >

    15. < mods:subject >

      1. < mods:topic > Materials -- Testing -- Congresses </ mods:topic >

      </ mods:subject >

    16. < mods:subject >

      1. < mods:topic > Indústria aeronàutica -- Congressos </ mods:topic >

      </ mods:subject >

    17. < mods:subject >

      1. < mods:topic > Aircraft industry -- Congresses </ mods:topic >

      </ mods:subject >

    18. < mods:titleInfo >

      1. < mods:title > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ mods:title >

      </ mods:titleInfo >

    19. < mods:genre > slide </ mods:genre >

    </ mods:mods >

oai_datacite

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < datacite:resource schemaLocation =" http://datacite.org/schema/kernel-4 http://schema.datacite.org/meta/kernel-4-2/metadata.xsd " >

    1. < datacite:identifier identifierType =" Handle " > http://hdl.handle.net/10256/23111 </ datacite:identifier >

    2. < datacite:titles >

      1. < datacite:title > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ datacite:title >

      </ datacite:titles >

    3. < datacite:creators >

      1. < datacite:creator >

        1. < datacite:creatorName > Castanié, Bruno </ datacite:creatorName >

        </ datacite:creator >

      2. < datacite:creator >

        1. < datacite:creatorName > Passieux, Jean-Charles </ datacite:creatorName >

        </ datacite:creator >

      3. < datacite:creator >

        1. < datacite:creatorName > Périé, Jean-Noel </ datacite:creatorName >

        </ datacite:creator >

      4. < datacite:creator >

        1. < datacite:creatorName > Bouvet, Christophe </ datacite:creatorName >

        </ datacite:creator >

      5. < datacite:creator >

        1. < datacite:creatorName > Serra, Joël </ datacite:creatorName >

        </ datacite:creator >

      </ datacite:creators >

    4. < datacite:contributors />
    5. < datacite:subjects >

      1. < datacite:subject > Assaigs de materials -- Congressos </ datacite:subject >

      2. < datacite:subject > Materials -- Testing -- Congresses </ datacite:subject >

      3. < datacite:subject > Indústria aeronàutica -- Congressos </ datacite:subject >

      4. < datacite:subject > Aircraft industry -- Congresses </ datacite:subject >

      </ datacite:subjects >

    6. < datacite:descriptions >

      1. < datacite:description descriptionType =" Abstract " > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ datacite:description >

      </ datacite:descriptions >

    7. < datacite:dates >

      1. < datacite:date dateType =" Issued " > 2023-05-31 </ datacite:date >

      </ datacite:dates >

    8. < datacite:publicationYear > 2023 </ datacite:publicationYear >

    9. < datacite:resourceType resourceTypeGeneral =" Dataset " />
    10. < datacite:languages >

      1. < datacite:language > eng </ datacite:language >

      </ datacite:languages >

    11. < datacite:relatedIdentifiers />
    12. < datacite:rightsList >

      1. < datacite:rights > Tots els drets reservats </ datacite:rights >

      2. < datacite:rights rightsURI =" info:eu-repo/semantics/openAccess " > info:eu-repo/semantics/openAccess </ datacite:rights >

      </ datacite:rightsList >

    13. < datacite:formats >

      1. < datacite:format > application/pdf </ datacite:format >

      </ datacite:formats >

    14. < datacite:publisher > Universitat de Girona. Grup de Recerca en Anàlisi i Materials Avançats per al Disseny Estructural (AMADE) </ datacite:publisher >

    </ datacite:resource >

ore

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < atom:entry schemaLocation =" http://www.w3.org/2005/Atom http://www.kbcafe.com/rss/atom.xsd.xml " >

    1. < atom:id > http://hdl.handle.net/10256/23111/ore.xml </ atom:id >

    2. < atom:link href =" http://hdl.handle.net/10256/23111 " rel =" alternate " />
    3. < atom:link href =" http://hdl.handle.net/10256/23111/ore.xml " rel =" http://www.openarchives.org/ore/terms/describes " />
    4. < atom:link href =" http://hdl.handle.net/10256/23111/ore.xml#atom " rel =" self " type =" application/atom+xml " />
    5. < atom:published > 2023-06-23T11:15:45Z </ atom:published >

    6. < atom:updated > 2023-06-23T11:15:45Z </ atom:updated >

    7. < atom:source >

      1. < atom:generator > DUGiDocs </ atom:generator >

      </ atom:source >

    8. < atom:title > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ atom:title >

    9. < atom:author >

      1. < atom:name > Castanié, Bruno </ atom:name >

      </ atom:author >

    10. < atom:author >

      1. < atom:name > Passieux, Jean-Charles </ atom:name >

      </ atom:author >

    11. < atom:author >

      1. < atom:name > Périé, Jean-Noel </ atom:name >

      </ atom:author >

    12. < atom:author >

      1. < atom:name > Bouvet, Christophe </ atom:name >

      </ atom:author >

    13. < atom:author >

      1. < atom:name > Serra, Joël </ atom:name >

      </ atom:author >

    14. < atom:category label =" Aggregation " scheme =" http://www.openarchives.org/ore/terms/ " term =" http://www.openarchives.org/ore/terms/Aggregation " />
    15. < atom:category scheme =" http://www.openarchives.org/ore/atom/modified " term =" 2023-06-23T11:15:45Z " />
    16. < atom:category label =" DSpace Item " scheme =" http://www.dspace.org/objectModel/ " term =" DSpaceItem " />
    17. < atom:link href =" https://dugi-doc.udg.edu/bitstream/10256/23111/1/02-11-Or-R033-20230531.pdf " length =" 1726762 " rel =" http://www.openarchives.org/ore/terms/aggregates " title =" 02-11-Or-R033-20230531.pdf " type =" application/pdf " />
    18. < atom:link href =" https://dugi-doc.udg.edu/bitstream/10256/23111/2/R033+-+Castani%C3%A9.pdf " length =" 224481 " rel =" http://www.openarchives.org/ore/terms/aggregates " title =" R033 - Castanié.pdf " type =" application/pdf " />
    19. < oreatom:triples >

      1. < rdf:Description about =" http://hdl.handle.net/10256/23111/ore.xml#atom " >

        1. < rdf:type resource =" http://www.dspace.org/objectModel/DSpaceItem " />
        2. < dcterms:modified > 2023-06-23T11:15:45Z </ dcterms:modified >

        </ rdf:Description >

      2. < rdf:Description about =" https://dugi-doc.udg.edu/bitstream/10256/23111/3/license.txt " >

        1. < rdf:type resource =" http://www.dspace.org/objectModel/DSpaceBitstream " />
        2. < dcterms:description > LICENSE </ dcterms:description >

        </ rdf:Description >

      3. < rdf:Description about =" https://dugi-doc.udg.edu/bitstream/10256/23111/1/02-11-Or-R033-20230531.pdf " >

        1. < rdf:type resource =" http://www.dspace.org/objectModel/DSpaceBitstream " />
        2. < dcterms:description > ORIGINAL </ dcterms:description >

        </ rdf:Description >

      4. < rdf:Description about =" https://dugi-doc.udg.edu/bitstream/10256/23111/2/R033+-+Castani%C3%A9.pdf " >

        1. < rdf:type resource =" http://www.dspace.org/objectModel/DSpaceBitstream " />
        2. < dcterms:description > ORIGINAL </ dcterms:description >

        </ rdf:Description >

      </ oreatom:triples >

    </ atom:entry >

qdc

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < qdc:qualifieddc schemaLocation =" http://purl.org/dc/elements/1.1/ http://dublincore.org/schemas/xmls/qdc/2006/01/06/dc.xsd http://purl.org/dc/terms/ http://dublincore.org/schemas/xmls/qdc/2006/01/06/dcterms.xsd http://dspace.org/qualifieddc/ http://www.ukoln.ac.uk/metadata/dcmi/xmlschema/qualifieddc.xsd " >

    1. < dc:title > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ dc:title >

    2. < dc:creator > Castanié, Bruno </ dc:creator >

    3. < dc:creator > Passieux, Jean-Charles </ dc:creator >

    4. < dc:creator > Périé, Jean-Noel </ dc:creator >

    5. < dc:creator > Bouvet, Christophe </ dc:creator >

    6. < dc:creator > Serra, Joël </ dc:creator >

    7. < dc:subject > Assaigs de materials -- Congressos </ dc:subject >

    8. < dc:subject > Materials -- Testing -- Congresses </ dc:subject >

    9. < dc:subject > Indústria aeronàutica -- Congressos </ dc:subject >

    10. < dc:subject > Aircraft industry -- Congresses </ dc:subject >

    11. < dcterms:abstract > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ dcterms:abstract >

    12. < dcterms:issued > 2023-05-31 </ dcterms:issued >

    13. < dc:type > slide </ dc:type >

    14. < dc:identifier > http://hdl.handle.net/10256/23111 </ dc:identifier >

    15. < dc:language > eng </ dc:language >

    16. < dc:relation > CompTest 2023 </ dc:relation >

    17. < dc:rights > info:eu-repo/semantics/openAccess </ dc:rights >

    18. < dc:rights > Tots els drets reservats </ dc:rights >

    19. < dc:publisher > Universitat de Girona. Grup de Recerca en Anàlisi i Materials Avançats per al Disseny Estructural (AMADE) </ dc:publisher >

    </ qdc:qualifieddc >

rdf

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < rdf:RDF schemaLocation =" http://www.openarchives.org/OAI/2.0/rdf/ http://www.openarchives.org/OAI/2.0/rdf.xsd " >

    1. < ow:Publication about =" oai:dugi-doc.udg.edu:10256/23111 " >

      1. < dc:title > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ dc:title >

      2. < dc:creator > Castanié, Bruno </ dc:creator >

      3. < dc:creator > Passieux, Jean-Charles </ dc:creator >

      4. < dc:creator > Périé, Jean-Noel </ dc:creator >

      5. < dc:creator > Bouvet, Christophe </ dc:creator >

      6. < dc:creator > Serra, Joël </ dc:creator >

      7. < dc:subject > Assaigs de materials -- Congressos </ dc:subject >

      8. < dc:subject > Materials -- Testing -- Congresses </ dc:subject >

      9. < dc:subject > Indústria aeronàutica -- Congressos </ dc:subject >

      10. < dc:subject > Aircraft industry -- Congresses </ dc:subject >

      11. < dc:description > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ dc:description >

      12. < dc:date > 2023-06-23T11:15:45Z </ dc:date >

      13. < dc:date > 2023-06-23T11:15:45Z </ dc:date >

      14. < dc:date > 2023-05-31 </ dc:date >

      15. < dc:type > slide </ dc:type >

      16. < dc:identifier > http://hdl.handle.net/10256/23111 </ dc:identifier >

      17. < dc:language > eng </ dc:language >

      18. < dc:relation > CompTest 2023 </ dc:relation >

      19. < dc:rights > info:eu-repo/semantics/openAccess </ dc:rights >

      20. < dc:rights > Tots els drets reservats </ dc:rights >

      21. < dc:publisher > Universitat de Girona. Grup de Recerca en Anàlisi i Materials Avançats per al Disseny Estructural (AMADE) </ dc:publisher >

      </ ow:Publication >

    </ rdf:RDF >

xoai

Descarregar XML

    <?xml version="1.0" encoding="UTF-8" ?>

  1. < metadata schemaLocation =" http://www.lyncode.com/xoai http://www.lyncode.com/xsd/xoai.xsd " >

    1. < element name =" dc " >

      1. < element name =" contributor " >

        1. < element name =" author " >

          1. < element name =" none " >

            1. < field name =" value " > Castanié, Bruno </ field >

            2. < field name =" value " > Passieux, Jean-Charles </ field >

            3. < field name =" value " > Périé, Jean-Noel </ field >

            4. < field name =" value " > Bouvet, Christophe </ field >

            5. < field name =" value " > Serra, Joël </ field >

            </ element >

          </ element >

        </ element >

      2. < element name =" date " >

        1. < element name =" accessioned " >

          1. < element name =" none " >

            1. < field name =" value " > 2023-06-23T11:15:45Z </ field >

            </ element >

          </ element >

        2. < element name =" available " >

          1. < element name =" none " >

            1. < field name =" value " > 2023-06-23T11:15:45Z </ field >

            </ element >

          </ element >

        3. < element name =" issued " >

          1. < element name =" none " >

            1. < field name =" value " > 2023-05-31 </ field >

            </ element >

          </ element >

        </ element >

      3. < element name =" identifier " >

        1. < element name =" uri " >

          1. < element name =" none " >

            1. < field name =" value " > http://hdl.handle.net/10256/23111 </ field >

            </ element >

          </ element >

        </ element >

      4. < element name =" description " >

        1. < element name =" abstract " >

          1. < element name =" cat " >

            1. < field name =" value " > The VERTEX test bench was designed to fulfil the need of virtual testing in the framework of certification of aeronautical structures. Funding obtained in 2013 for a total amount of 3000 k€ made it possible to both fund the test rig design and manufacturing (500 k€) and initiate research. The choice of the design of the machine and the size of the specimen is based on a first experience of Castanié et al. [Exp. Mech. 44:5 (2004) 461–472]. The specimens are said to be technological in the sense that they do not represent a particular part of an aircraft but a technology and/or make it possible to study a scientific or industrial problem. In the first version, the area of interest (200 x 200mm2) proved to be too small and difficulties in finding the force and moment fluxes locally applied were raised. As a result, the area of interest was quadrupled (400 x 400 mm2) in VERTEX and a specific test/calculation dialogue had to be developed. VERTEX provides a low-cost solution for testing at an intermediate scale, representative of larger scale tests, to provide rapid feedback on new technologies and/or materials. The machine is mainly made up of a tubular box on which the specimen is bolted to complete the upper face of the central part. Jacks 1 and 2 can be pushed or pulled symmetrically to bend the box, locally creating tension or compression on the sample. Jacks 3 and 4 can be pushed to twist the centre of the box, locally creating shear on the sample. An air-pressurised rubber bladder can be added in the central box to load the sample with pressure. The four jacks and the bladder pressure can be controlled independently to apply combined structural loadings in tension/compression + shear + pressure on the sample </ field >

            </ element >

          </ element >

        2. < element name =" provenance " >

          1. < element name =" en " >

            1. < field name =" value " > Submitted by Claudia Plana (claudia.plana@udg.edu) on 2023-06-23T11:15:45Z No. of bitstreams: 2 02-11-Or-R033-20230531.pdf: 1726762 bytes, checksum: be15ffd16c35c24bf2b320d5e7e7274c (MD5) R033 - Castanié.pdf: 224481 bytes, checksum: be57f431673711d034109a723435cc3e (MD5) </ field >

            2. < field name =" value " > Made available in DSpace on 2023-06-23T11:15:45Z (GMT). No. of bitstreams: 2 02-11-Or-R033-20230531.pdf: 1726762 bytes, checksum: be15ffd16c35c24bf2b320d5e7e7274c (MD5) R033 - Castanié.pdf: 224481 bytes, checksum: be57f431673711d034109a723435cc3e (MD5) Previous issue date: 2023-05-31 </ field >

            </ element >

          </ element >

        </ element >

      5. < element name =" format " >

        1. < element name =" mimetype " >

          1. < element name =" cat " >

            1. < field name =" value " > application/pdf </ field >

            </ element >

          </ element >

        </ element >

      6. < element name =" language " >

        1. < element name =" iso " >

          1. < element name =" cat " >

            1. < field name =" value " > eng </ field >

            </ element >

          </ element >

        </ element >

      7. < element name =" publisher " >

        1. < element name =" cat " >

          1. < field name =" value " > Universitat de Girona. Grup de Recerca en Anàlisi i Materials Avançats per al Disseny Estructural (AMADE) </ field >

          </ element >

        </ element >

      8. < element name =" relation " >

        1. < element name =" ispartofseries " >

          1. < element name =" cat " >

            1. < field name =" value " > CompTest 2023 </ field >

            </ element >

          </ element >

        </ element >

      9. < element name =" rights " >

        1. < element name =" none " >

          1. < field name =" value " > Tots els drets reservats </ field >

          </ element >

        2. < element name =" accessRights " >

          1. < element name =" cat " >

            1. < field name =" value " > info:eu-repo/semantics/openAccess </ field >

            </ element >

          </ element >

        </ element >

      10. < element name =" subject " >

        1. < element name =" cat " >

          1. < field name =" value " > Assaigs de materials -- Congressos </ field >

          2. < field name =" value " > Materials -- Testing -- Congresses </ field >

          3. < field name =" value " > Indústria aeronàutica -- Congressos </ field >

          4. < field name =" value " > Aircraft industry -- Congresses </ field >

          </ element >

        </ element >

      11. < element name =" title " >

        1. < element name =" cat " >

          1. < field name =" value " > 2013-2023: ten years of experimental, numerical and measurement developments with the vertex multiaxial test bench </ field >

          </ element >

        </ element >

      12. < element name =" type " >

        1. < element name =" cat " >

          1. < field name =" value " > slide </ field >

          </ element >

        </ element >

      </ element >

    2. < element name =" adm " >

      1. < element name =" sets " >

        1. < element name =" hidden " >

          1. < element name =" cat " >

            1. < field name =" value " > rc1 </ field >

            </ element >

          </ element >

        </ element >

      </ element >

    3. < element name =" bundles " >

      1. < element name =" bundle " >

        1. < field name =" name " > LICENSE </ field >

        2. < element name =" bitstreams " >

          1. < element name =" bitstream " >

            1. < field name =" name " > license.txt </ field >

            2. < field name =" originalName " > license.txt </ field >

            3. < field name =" format " > text/plain </ field >

            4. < field name =" size " > 1748 </ field >

            5. < field name =" url " > https://dugi-doc.udg.edu/bitstream/10256/23111/3/license.txt </ field >

            6. < field name =" checksum " > 8a4605be74aa9ea9d79846c1fba20a33 </ field >

            7. < field name =" checksumAlgorithm " > MD5 </ field >

            8. < field name =" sid " > 3 </ field >

            </ element >

          </ element >

        </ element >

      2. < element name =" bundle " >

        1. < field name =" name " > ORIGINAL </ field >

        2. < element name =" bitstreams " >

          1. < element name =" bitstream " >

            1. < field name =" name " > 02-11-Or-R033-20230531.pdf </ field >

            2. < field name =" originalName " > 02-11-Or-R033-20230531.pdf </ field >

            3. < field name =" description " />
            4. < field name =" format " > application/pdf </ field >

            5. < field name =" size " > 1726762 </ field >

            6. < field name =" url " > https://dugi-doc.udg.edu/bitstream/10256/23111/1/02-11-Or-R033-20230531.pdf </ field >

            7. < field name =" checksum " > be15ffd16c35c24bf2b320d5e7e7274c </ field >

            8. < field name =" checksumAlgorithm " > MD5 </ field >

            9. < field name =" sid " > 1 </ field >

            </ element >

          2. < element name =" bitstream " >

            1. < field name =" name " > R033 - Castanié.pdf </ field >

            2. < field name =" originalName " > R033 - Castanié.pdf </ field >

            3. < field name =" description " />
            4. < field name =" format " > application/pdf </ field >

            5. < field name =" size " > 224481 </ field >

            6. < field name =" url " > https://dugi-doc.udg.edu/bitstream/10256/23111/2/R033+-+Castani%C3%A9.pdf </ field >

            7. < field name =" checksum " > be57f431673711d034109a723435cc3e </ field >

            8. < field name =" checksumAlgorithm " > MD5 </ field >

            9. < field name =" sid " > 2 </ field >

            </ element >

          </ element >

        </ element >

      </ element >

    4. < element name =" others " >

      1. < field name =" handle " > 10256/23111 </ field >

      2. < field name =" identifier " > oai:dugi-doc.udg.edu:10256/23111 </ field >

      3. < field name =" lastModifyDate " > 2023-06-23 13:15:45.132 </ field >

      </ element >

    5. < element name =" repository " >

      1. < field name =" name " > DUGiDocs </ field >

      2. < field name =" mail " > oriol.olive@udg.edu </ field >

      </ element >

    6. < element name =" license " >

      1. < field name =" bin " > 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 </ field >

      </ element >

    </ metadata >

Biblioteca de Catalunya Carrer de l'Hospital, 56. 08001 Barcelona Adreça electrònica: catalonica@bnc.cat Tlf.: +34 932 702 300
  • Logotipo de Biblioteca de Catalunya
  • Logotipo de la Generalitat de Catalunya
  • Nota tècnica
  • Avís legal
  • Repositori OAI