Please use this identifier to cite or link to this item:
http://bura.brunel.ac.uk/handle/2438/17333
Title: | Conceptual advanced transport aircraft design configuration for sustained hypersonic flight |
Authors: | Alkaya, C Sam, AA Pesyridis, A |
Keywords: | hypersonic aircraft;CFD; preliminary design |
Issue Date: | 2018 |
Citation: | Aerospace, 2018, 5 (3) |
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. |
URI: | http://bura.brunel.ac.uk/handle/2438/17333 |
DOI: | http://dx.doi.org/10.3390/aerospace5030091 |
ISSN: | http://dx.doi.org/10.3390/aerospace5030091 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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