Please use this identifier to cite or link to this item:
http://bura.brunel.ac.uk/handle/2438/17068
Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Tang, J | - |
dc.contributor.author | Kanfoud, J | - |
dc.contributor.author | Mares, C | - |
dc.contributor.author | Soua, S | - |
dc.coverage.spatial | 2–4 July 2018, Clare College, Cambridge, United Kingdom | - |
dc.date.accessioned | 2018-11-08T15:00:35Z | - |
dc.date.available | 2018-11-06 | - |
dc.date.available | 2018-11-08T15:00:35Z | - |
dc.date.issued | 2018 | - |
dc.identifier.citation | http://iopscience.iop.org/issue/1742-6596/1106, 2018, 1106 | en_US |
dc.identifier.issn | http://dx.doi.org/10.1088/1742-6596/1106/1/012016 | - |
dc.identifier.uri | http://bura.brunel.ac.uk/handle/2438/17068 | - |
dc.description.abstract | Due to the complexity of composite material, accurate manufacturing is very complicated and carry over a large number of uncertainties, the process of optimization and In this paper as part of design technology for rotor blades, the process of mechanical testing against severe working conditions using Acoustic Emission (AE) is discussed. As part of this process, the dynamic behaviour is analysed with validation and model updating of the structure and material properties, followed by structural tests under loads specific to the operational conditions. The results presented show how the appropriate AE technique has been implemented in order to obtain relevant data and focus on specific areas of interest for the design development, for correlation between modelling and experimental testing, the structure being tested to the ultimate load. | en_US |
dc.language.iso | en | en_US |
dc.publisher | IOP Publishing | en_US |
dc.relation.ispartofseries | 1106;012016 | - |
dc.source | Modern Practice in Stress and Vibration Analysis (MPSVA) 2018 | - |
dc.source | Modern Practice in Stress and Vibration Analysis (MPSVA) 2018 | - |
dc.subject | Acoustic emission | en_US |
dc.subject | Composites | en_US |
dc.subject | Resonance Frequency | en_US |
dc.subject | Tensile | en_US |
dc.subject | Flexion | en_US |
dc.title | Destructive Testing of Open Rotor Propeller Blades for Extreme Operation Conditions | en_US |
dc.type | Conference Paper | en_US |
dc.identifier.doi | http://dx.doi.org/10.1088/1742-6596/1106/1/012016 | - |
dc.relation.isPartOf | http://iopscience.iop.org/issue/1742-6596/1106 | - |
pubs.finish-date | 2018-07-04 | - |
pubs.finish-date | 2018-07-04 | - |
pubs.publication-status | Published | - |
pubs.start-date | 2018-07-02 | - |
pubs.start-date | 2018-07-02 | - |
pubs.volume | 1106 | - |
Appears in Collections: | Dept of Mechanical and Aerospace Engineering Research Papers |
Files in This Item:
File | Description | Size | Format | |
---|---|---|---|---|
Fulltext.pdf | 1.43 MB | Adobe PDF | View/Open |
Items in BURA are protected by copyright, with all rights reserved, unless otherwise indicated.