Computer-aided conceptual aircraft design (CACAD) for transport aircraft

dc.contributor.authorVaziry-Zanjany , Mohammad Ali (F)en_UK
dc.date1996en_UK
dc.date.accessioned2005-11-23T12:20:35Z
dc.date.available2005-11-23T12:20:35Z
dc.date.issued1996en_UK
dc.description.abstractCACAD is capable to optimise the size, and configurations of turbofab-powered transport aircraft. The synthesis sizes aircraft from the low-capacity short range Fokker F-100 class to the long range medium-capacity Airbus A-340 class. It has an optimisation capability, with the objective function being direct operating cost in which, maintenance costs is extensively sub-divided according to ATA chapters. The objective of this report is to present the listing, the user's guide on how to run the program, as well as the description of the formulation used within the program. There are flow charts, table of nomenclatures included in this report. The floppy disc that contains the programme listings will be made available on request from the office of Department of Aerospace Technology, College of Aeronautics, Cranfield University, Cranfield, Bedford, UK, MK43 0ALen_UK
dc.description.sponsorshipThe Universityen_UK
dc.format.extent1963 bytes
dc.format.extent6589050 bytes
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.identifier.urihttp://hdl.handle.net/1826/196
dc.language.isoen_UKen_UK
dc.relation.ispartofseriesCollege of Aeronautics Report;9608en_UK
dc.relation.ispartofseriesCU/CoA/R;9608en_UK
dc.titleComputer-aided conceptual aircraft design (CACAD) for transport aircraften_UK
dc.typeTechnical Reporten_UK

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