dc.creator |
Sepulveda, Eduardo |
|
dc.creator |
Smith, Howard |
|
dc.creator |
Sziroczak, David |
|
dc.date |
2018-09-13T12:48:00Z |
|
dc.date |
2018-09-13T12:48:00Z |
|
dc.date |
2018-08-01 |
|
dc.date.accessioned |
2022-05-25T16:38:28Z |
|
dc.date.available |
2022-05-25T16:38:28Z |
|
dc.identifier |
E. Sepulveda, H. Smith and D. Sziroczak. Multidisciplinary analysis of subsonic stealth unmanned combat aerial vehicles. CEAS Aeronautical Journal, Volume 10, Issue 2, June 2019, pp. 431-442 |
|
dc.identifier |
1869-5582 |
|
dc.identifier |
https://doi.org/10.1007/s13272-018-0325-0 |
|
dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/13482 |
|
dc.identifier.uri |
http://localhost:8080/xmlui/handle/CUHPOERS/182338 |
|
dc.description |
In this paper, the GENUS multidisciplinary aircraft design and analysis environment is presented in its application to the conceptual design of tailless, low-observable unmanned combat aerial vehicles (UCAVs). Analysis disciplines comprise a variety of low to medium fidelity, physics-based and empirical methodologies, as well as higher order panel method aerodynamic analysis. Stealth considerations have been included in terms of a radar cross section analysis through a physical optics approximation method, with results verified against a well-known radar cross section prediction code. Preliminary results show good agreement for gross and empty masses when compared to several existing UCAV demonstrators and conceptual designs. A further validation of the presented methodologies is evaluated through the design, analysis, and optimisation of an unmanned strike fighter concept. |
|
dc.language |
en |
|
dc.publisher |
Springer |
|
dc.rights |
Attribution 4.0 International |
|
dc.rights |
http://creativecommons.org/licenses/by/4.0/ |
|
dc.subject |
UCAV |
|
dc.subject |
Stealth |
|
dc.subject |
Conceptual design |
|
dc.subject |
Tailless aircraft |
|
dc.subject |
UAV |
|
dc.title |
Multidisciplinary analysis of subsonic stealth unmanned combat aerial vehicles |
|
dc.type |
Article |
|