Set-based approach to passenger aircraft family design
dc.contributor.author | Riaz, Atif | |
dc.contributor.author | Guenov, Marin D. | |
dc.contributor.author | Molina-Cristobal, Arturo | |
dc.date.accessioned | 2016-10-21T10:38:07Z | |
dc.date.available | 2016-10-21T10:38:07Z | |
dc.date.issued | 2016-09-13 | |
dc.description.abstract | Presented is a method for the design of passenger aircraft families. Existing point-based methods found in the literature employ sequential approaches in which a single design solution is selected early and is then iteratively modified until all requirements are satisfied. The challenge with such approaches is that the design is driven toward a solution that, although promising to the optimizer, may be infeasible due to factors not considered by the models. The proposed method generates multiple solutions at the outset. Then, the infeasible solutions are discarded gradually through constraint satisfaction and set intersection. The method has been evaluated through a notional example of a three-member aircraft family design. The conclusion is that point-based design is still seen as preferable for incremental (conventional) designs based on a wealth of validated empirical methods, whereas the proposed approach, although resource-intensive, is seen as more suited to innovative designs. | en_UK |
dc.identifier.citation | Riaz A, Guenov MD, Molina-Cristobal A, Set-based approach to passenger aircraft family design, Journal of Aircraft, Volume 54, Issue 1, 2017 | en_UK |
dc.identifier.cris | 15454750 | |
dc.identifier.issn | 0021-8669 | |
dc.identifier.uri | http://dx.doi.org/10.2514/1.C033747 | |
dc.identifier.uri | https://dspace.lib.cranfield.ac.uk/handle/1826/10820 | |
dc.language.iso | en | en_UK |
dc.publisher | American Institute of Aeronautics and Astronautics | en_UK |
dc.rights | Attribution-NonCommercial 4.0 International | |
dc.rights.uri | http://creativecommons.org/licenses/by-nc/4.0/ | |
dc.title | Set-based approach to passenger aircraft family design | en_UK |
dc.type | Article | en_UK |
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