Bonded Repair of Aircraft Structures:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Dordrecht
Springer Netherlands
1988
|
| Schriftenreihe: | Engineering Application of Fracture Mechanics
7 |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Beschreibung: | The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significance, (iii) forecasting future behaviour-prognosis, and (iv) pre scription and implementation of remedial measures including repairs. Considerable scientific effort has been devoted to developing the science and technology base for the first three phases. Of particular note is the development of fracture mechanics as a major analytical tool for metals, for predicting residual strength in the presence of cracks ( damage tolerance) and rate of crack propagation under service loading. Intensive effort is currently being devoted to developing similar approaches for fibre composite structures, particularly to assess damage tolerance and durability in the presence of delamination damage. Until recently there has been no major attempt to develop a science and tech nology base for the last phase, particularly with respect to the development of repairs. Approaches are required which will allow assessment of the type and magnitude of defects amenable to repair and the influence of the repair on the stress intensity factor (or some related parameter). Approaches are also required for the development and design of optimum repairs and for assessment of their durability |
| Beschreibung: | 1 Online-Ressource (XIII, 214 p) |
| ISBN: | 9789400927520 9789401077361 |
| DOI: | 10.1007/978-94-009-2752-0 |
Internformat
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| 100 | 1 | |a Baker, A. A. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Bonded Repair of Aircraft Structures |c edited by A. A. Baker, R. Jones |
| 264 | 1 | |a Dordrecht |b Springer Netherlands |c 1988 | |
| 300 | |a 1 Online-Ressource (XIII, 214 p) | ||
| 336 | |b txt |2 rdacontent | ||
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| 490 | 0 | |a Engineering Application of Fracture Mechanics |v 7 | |
| 500 | |a The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significance, (iii) forecasting future behaviour-prognosis, and (iv) pre scription and implementation of remedial measures including repairs. Considerable scientific effort has been devoted to developing the science and technology base for the first three phases. Of particular note is the development of fracture mechanics as a major analytical tool for metals, for predicting residual strength in the presence of cracks ( damage tolerance) and rate of crack propagation under service loading. Intensive effort is currently being devoted to developing similar approaches for fibre composite structures, particularly to assess damage tolerance and durability in the presence of delamination damage. Until recently there has been no major attempt to develop a science and tech nology base for the last phase, particularly with respect to the development of repairs. Approaches are required which will allow assessment of the type and magnitude of defects amenable to repair and the influence of the repair on the stress intensity factor (or some related parameter). Approaches are also required for the development and design of optimum repairs and for assessment of their durability | ||
| 650 | 4 | |a Engineering | |
| 650 | 4 | |a Automotive Engineering | |
| 650 | 4 | |a Ingenieurwissenschaften | |
| 700 | 1 | |a Jones, R. |e Sonstige |4 oth | |
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Datensatz im Suchindex
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| author_facet | Baker, A. A. |
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| building | Verbundindex |
| bvnumber | BV042415035 |
| classification_tum | PHY 000 |
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| dewey-full | 629.2 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.2 |
| dewey-search | 629.2 |
| dewey-sort | 3629.2 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Physik Verkehr / Transport |
| doi_str_mv | 10.1007/978-94-009-2752-0 |
| format | Electronic eBook |
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| id | DE-604.BV042415035 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-10T01:20:56Z |
| institution | BVB |
| isbn | 9789400927520 9789401077361 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-027850528 |
| oclc_num | 863769973 |
| open_access_boolean | |
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| owner_facet | DE-91 DE-BY-TUM DE-83 |
| physical | 1 Online-Ressource (XIII, 214 p) |
| psigel | ZDB-2-PHA ZDB-2-BAE ZDB-2-PHA_Archive |
| publishDate | 1988 |
| publishDateSearch | 1988 |
| publishDateSort | 1988 |
| publisher | Springer Netherlands |
| record_format | marc |
| series2 | Engineering Application of Fracture Mechanics |
| spelling | Baker, A. A. Verfasser aut Bonded Repair of Aircraft Structures edited by A. A. Baker, R. Jones Dordrecht Springer Netherlands 1988 1 Online-Ressource (XIII, 214 p) txt rdacontent c rdamedia cr rdacarrier Engineering Application of Fracture Mechanics 7 The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significance, (iii) forecasting future behaviour-prognosis, and (iv) pre scription and implementation of remedial measures including repairs. Considerable scientific effort has been devoted to developing the science and technology base for the first three phases. Of particular note is the development of fracture mechanics as a major analytical tool for metals, for predicting residual strength in the presence of cracks ( damage tolerance) and rate of crack propagation under service loading. Intensive effort is currently being devoted to developing similar approaches for fibre composite structures, particularly to assess damage tolerance and durability in the presence of delamination damage. Until recently there has been no major attempt to develop a science and tech nology base for the last phase, particularly with respect to the development of repairs. Approaches are required which will allow assessment of the type and magnitude of defects amenable to repair and the influence of the repair on the stress intensity factor (or some related parameter). Approaches are also required for the development and design of optimum repairs and for assessment of their durability Engineering Automotive Engineering Ingenieurwissenschaften Jones, R. Sonstige oth https://doi.org/10.1007/978-94-009-2752-0 Verlag Volltext |
| spellingShingle | Baker, A. A. Bonded Repair of Aircraft Structures Engineering Automotive Engineering Ingenieurwissenschaften |
| title | Bonded Repair of Aircraft Structures |
| title_auth | Bonded Repair of Aircraft Structures |
| title_exact_search | Bonded Repair of Aircraft Structures |
| title_full | Bonded Repair of Aircraft Structures edited by A. A. Baker, R. Jones |
| title_fullStr | Bonded Repair of Aircraft Structures edited by A. A. Baker, R. Jones |
| title_full_unstemmed | Bonded Repair of Aircraft Structures edited by A. A. Baker, R. Jones |
| title_short | Bonded Repair of Aircraft Structures |
| title_sort | bonded repair of aircraft structures |
| topic | Engineering Automotive Engineering Ingenieurwissenschaften |
| topic_facet | Engineering Automotive Engineering Ingenieurwissenschaften |
| url | https://doi.org/10.1007/978-94-009-2752-0 |
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