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http://bura.brunel.ac.uk/handle/2438/17333
Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Alkaya, C | - |
dc.contributor.author | Sam, AA | - |
dc.contributor.author | Pesyridis, A | - |
dc.date.accessioned | 2019-01-11T16:44:39Z | - |
dc.date.available | 2018-09-01 | - |
dc.date.available | 2019-01-11T16:44:39Z | - |
dc.date.issued | 2018 | - |
dc.identifier.citation | Aerospace, 2018, 5 (3) | en_US |
dc.identifier.issn | http://dx.doi.org/10.3390/aerospace5030091 | - |
dc.identifier.issn | 2226-4310 | - |
dc.identifier.uri | http://bura.brunel.ac.uk/handle/2438/17333 | - |
dc.description.abstract | © 2018 by the authors. The conceptual aircraft design and its integration with a combined cycle engine for hypersonic cruise at Mach 8 is documented in this paper. The paper describes the process taken to develop a hypersonic aircraft from a conceptual approach. The discussion also includes the design and CFD analysis of the integrated combined cycle engine. A final conceptual hypersonic transport aircraft with an integrated combined cycle engine was achieved through this study. According to the analysis carried out, the aircraft is able to take-off and land at the airports it is intended to be used and will be able to generate enough thrust to sustain hypersonic cruise at an altitude of 30 km. | en_US |
dc.language.iso | en | en_US |
dc.subject | hypersonic aircraft | en_US |
dc.subject | CFD; preliminary design | en_US |
dc.title | Conceptual advanced transport aircraft design configuration for sustained hypersonic flight | en_US |
dc.type | Article | en_US |
dc.identifier.doi | http://dx.doi.org/10.3390/aerospace5030091 | - |
dc.relation.isPartOf | Aerospace | - |
pubs.issue | 3 | - |
pubs.publication-status | Published | - |
pubs.volume | 5 | - |
dc.identifier.eissn | 2226-4310 | - |
Appears in Collections: | Aeronautics |
Files in This Item:
File | Description | Size | Format | |
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Fulltext.docx | 3.79 MB | Microsoft Word XML | View/Open |
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